#=======================================================================
# @(#) $Id$
#-----------------------------------------------------------------------
#
########################################################################
#  MATERIALS LIBRARY FOR CFX-5
########################################################################
#
#  This file includes the CCL description of materials supplied as part
#  of the CFX-5 installation. Note that the default materials are defined
#  in MATERIALS-default.ccl
#
########################################################################
#  Description:
#
#  MATERIAL : <name>
#    Option = Pure Substance
#    Thermodynamic State = <Solid|Liquid|Gas>
#    PROPERTIES:
#      Option = General Material
#      EQUATION OF STATE:
#        Option = Ideal Gas
#        Molar Mass = <Real>
#      END
#      SPECIFIC HEAT CAPACITY:
#        Option = Value
#        Specific Heat Capacity = <Real>
#      END
#      DYNAMIC VISCOSITY:
#        Option = Value
#        Dynamic Viscosity = <Real>
#      END
#      THERMAL CONDUCTIVITY:
#        Option = Value
#        Thermal Conductivity = <Real>
#      END
#      ABSORPTION COEFFICIENT:
#        Option = Value
#        Absorption Coefficient = <Real>
#      END
#      SCATTERING COEFFICIENT:
#        Option = Value
#        Scattering Coefficient = <Real>
#      END
#      REFRACTIVE INDEX:
#        Option = Value
#        Refractive Index = <Real>
#      END
#    END
#  END
#
# Notice for SPECIFIC HEAT CAPACITY
#
#   The NASA SP-273 format states that Upper Range Coefficients are 
#   listed first, and Lower Range are listed second. The format used
#   by CFX-5 before CFX-5.7 follows this to the letter.
#
#   To create a new CFX-5.7 material, copy and paste the 3 lines
#   (14's coef's) from your database and insert comas to separate
#   the coefficients.
#
#   Similar for the Temperature Limit List.
#
#   Load the CCL into CFX-Pre and it will automatically be upgraded
#   to the new CFX-5.7 materials format.
#
#   CFX-5.6 NASA format specific heat looks as follows:
#
#     SPECIFIC HEAT CAPACITY:
#       Option = NASA Format
#       Temperature Limit List = 300 [K], 5000 [K], 1000 [K]
#       NASA Coefficient List = \
#            0.02500000E+02,  0.00000000E+00,  0.00000000E+00, \
#            0.00000000E+00,  0.00000000E+00, -0.07453750E+04, \
#            0.04366001E+02, \
#            0.02500000E+02,  0.00000000E+00,  0.00000000E+00, \
#            0.00000000E+00,  0.00000000E+00, -0.07453750E+04, \
#            0.04366001E+02
#    END # SPECIFIC HEAT CAPACITY
#
########################################################################
#
#  File Structure
#
#  The file is split into the following pieces:
#    - Air data
#    - Water and water vapour data (self-consistent)
#    - Gases (NASA SP-273 data for Cp, h and s)
#    - Gases (Constant density and Cp)
#    - Gases (Ideal gas equation of state, Constant Cp)
#    - Liquids
#    - Solids
#
#  Note that, in general, these materials do not have the reference
#  data points, and may therefore not be mixed (eg, combustion, 
#  phase change).  However, the water data is consistent with the NASA
#  gases, so those materials may be mixed.
#
########################################################################

LIBRARY:

########################################################################
# Air data (also refer to MATERIALS-default.ccl
########################################################################

  MATERIAL:Air at STP
    Material Description = Air at STP (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Air Data, Constant Property Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 1.725E-05 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 0.01 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 2.428E-02 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 1.284 [kg m^-3]
        Molar Mass = 28.96 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1.0038E+03 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = 0. [J/kg]
        Reference Specific Entropy = 0. [J/kg/K]
        Reference Temperature = 0 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 0.00366 [K^-1]
      END
    END
  END

########################################################################
# Water data - also refer to MATERIALS-default.ccl
########################################################################

# The data for these materials are from the NIST Chemistry WebBook.
# The Reference Specific Enthalpy data are changed to be consistent
# with NASA coefficient enthalpy and entropy data.
#
# In this case the reference enthalpy of -1.5866449E+7 [J/kg] is 
# offset from the NASA H2O enthalpy value hgas(298.15 K) by 
# hfg = -2441.42E3 J/kg.
#
# The entropy is similary offset from the gas value at at the
# liquid phase reference conditions, sgas(298.15,3.169 kPa)
# s_liquid_ref = sgas(298.15,3.169 kPa) - hfg/298.15 K
#


  MATERIAL:Water at 25 C
    Material Description = Water (saturated liquid) at 25 C
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Water Data, Constant Property Liquids, \
                     Interphase Mass Transfer
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 8.899E-4 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.6069 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 997.0 [kg m^-3]
        Molar Mass = 18.02 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 4181.7 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Specific Enthalpy = -1.5866449E+7 [J/kg]
        Reference Specific Entropy = 2.82482E+03 [J/kg/K]	   	   
        Reference Temperature = 25 [C]
        Reference Pressure = 3.169E-2 [bar]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 2.57E-04 [K^-1]
      END
    END
  END

  MATERIAL:Water Vapour at 25 C
    Material Description = Water (saturated vapour) at 25 C
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Water Data, Constant Property Gases, \
                     Interphase Mass Transfer
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 9.8626E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.01854 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 0.02308 [kg m^-3]
        Molar Mass = 18.02 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1911.6 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 3.169E-2 [bar]
#       Reference Specific Enthalpy = 2.547E+6 [J/kg]  (NIST)
        Reference Specific Enthalpy = -1.3424249E+7 [J/kg]
        Reference Specific Entropy = 1.0475125E+04 [J/kg/K]
        Reference Temperature = 25 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 0.003356 [K^-1]
      END
    END
  END

  MATERIAL:Water Vapour at 100 C
    Material Description = Water (saturated vapour) at 100 C
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Water Data, Constant Property Gases, \
                     Interphase Mass Transfer
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 1.2270E-05 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.02510 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 0.59837 [kg m^-3]
        Molar Mass = 18.02 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2080.1 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1.014 [bar]
#       Reference Specific Enthalpy = 2.676E+6 [J/kg]  (NIST)
        Reference Specific Enthalpy = -1.3295249E+7 [J/kg]
        Reference Specific Entropy = 1.0896275E+04 [J/kg/K]
        Reference Temperature = 100 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 2.68e-03 [K^-1]
      END
    END
  END

  MATERIAL:Water at 100 C
    Material Description = Water (saturated liquid) at 100 C
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Water Data, Constant Property Liquids, \
                     Interphase Mass Transfer
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 2.817E-4 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.6791 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 958.4 [kg m^-3]
        Molar Mass = 18.02 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 4215.7 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1.014 [bar]
#       Reference Specific Enthalpy = 4.192E+5 [J/kg]  (NIST)
        Reference Specific Enthalpy = -1.5552049E+7 [J/kg]
        Reference Specific Entropy = 4.8215097E+03 [J/kg/K]
        Reference Temperature = 100 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 7.4E-04 [K^-1]
      END
    END
  END

########################################################################
# Ideal gases using NASA SP-273 Format Properties (Cp, H, S)
########################################################################
#
#  Thermodynamic data for these materials was obtained from:
#
#  Kee,R. J.,Rupley,F. M.,Miller,J. A.,"Chemkin-II: A Fortran
#  Chemical Kinetics Package for the Analysis of Gas-Phase Chemical
#  Kinetics," Sandia National Laboratories Report,SAND89-8009,(1991)

  MATERIAL:Ar
    Material Description = Argon Ar 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.02500000E+02 []
          NASA a2 = 0.00000000E+00 [K^-1]
          NASA a3 = 0.00000000E+00 [K^-2]
          NASA a4 = 0.00000000E+00 [K^-3]
          NASA a5 = 0.00000000E+00 [K^-4]
          NASA a6 = -0.07453750E+04 [K]
          NASA a7 = 0.04366001E+02 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.02500000E+02 []
          NASA a2 = 0.00000000E+00 [K^-1]
          NASA a3 = 0.00000000E+00 [K^-2]
          NASA a4 = 0.00000000E+00 [K^-3]
          NASA a5 = 0.00000000E+00 [K^-4]
          NASA a6 = -0.07453750E+04 [K]
          NASA a7 = 0.04366001E+02 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 23.9E-6 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 180E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 39.95 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END
 
  MATERIAL:CCl4	   
    Material Description = Tetrachloromethane Vapour (CCl4)	   
    Option = Pure Substance	   
    Thermodynamic State = Gas	   
    Material Group = Gas Phase Combustion	   
    PROPERTIES:	   
      Option = General Material	   
      SPECIFIC HEAT CAPACITY:	   
        Option = NASA Format	   
        TEMPERATURE LIMITS:	   
          Lower Temperature = 298.15 [K]	   
          Midpoint Temperature = 1000 [K]	   
          Upper Temperature = 5000 [K]	   
        END	   
        LOWER INTERVAL COEFFICIENTS:	   
          NASA a1 = 5.79662990E+00 []	   
          NASA a2 = 1.79774390E-02 [K^-1]	   
          NASA a3 = -1.09565460E-05 [K^-2]	   
          NASA a4 = -6.66818070E-09 [K^-3]	   
          NASA a5 = 6.45548980E-12 [K^-4]	   
          NASA a6 = -1.39409650E+04 [K]	   
          NASA a7 = -5.70110920E-01 []	   
        END	   
        UPPER INTERVAL COEFFICIENTS:	   
          NASA a1 = 1.17390960E+01 []	   
          NASA a2 = 1.28375530E-03 [K^-1]	   
          NASA a3 = -4.96502590E-07 [K^-2]	   
          NASA a4 = 8.35250200E-11 [K^-3]	   
          NASA a5 = -5.11072240E-15 [K^-4]	   
          NASA a6 = -1.54190900E+04 [K]	   
          NASA a7 = -3.07909700E+01 []	   
        END	   
      END	   
      REFERENCE STATE:	   
        Option = NASA Format	   
        Reference Pressure = 1 [atm]	   
        Reference Temperature =  298.15 [K]	   
      END      	   
      DYNAMIC VISCOSITY:	   
        Dynamic Viscosity = 0.000020602 [kg/m/s]	   
        Option = Value	   
      END	   
      REFRACTIVE INDEX:	   
        Option = Value	   
        Refractive Index = 1 [m m^-1]	   
      END	   
      SCATTERING COEFFICIENT:	   
        Option = Value	   
        Scattering Coefficient = 0 [m^-1]	   
      END	   
      ABSORPTION COEFFICIENT:	   
        Absorption Coefficient = 1 [m^-1]	   
        Option = Value	   
      END	   
      THERMAL CONDUCTIVITY:	   
        Option = Value	   
        Thermal Conductivity = 0.015116 [W m^-1 K^-1]	   
      END	   
      EQUATION OF STATE:	   
        Molar Mass = 153.822 [kg kmol^-1]	   
        Option = Ideal Gas	   
      END	   
    END	   
  END	   
	   
  MATERIAL:CF4	   
    Material Description = Tetrafluoromethane Vapour (CF4)	   
    Option = Pure Substance	   
    Thermodynamic State = Gas	   
    Material Group = Gas Phase Combustion	   
    PROPERTIES:	   
      Option = General Material	   
      SPECIFIC HEAT CAPACITY:	   
        Option = NASA Format	   
        TEMPERATURE LIMITS:	   
          Lower Temperature = 200 [K]	   
          Midpoint Temperature = 1000 [K]	   
          Upper Temperature = 6000 [K]	   
        END	   
        LOWER INTERVAL COEFFICIENTS:	   
          NASA a1 = 1.05119594E+00 []	   
          NASA a2 = 2.78318369E-02 [K^-1]	   
          NASA a3 = -2.46683439E-05 [K^-2]	   
          NASA a4 = 6.75882532E-09 [K^-3]	   
          NASA a5 = 9.14850873E-13 [K^-4]	   
          NASA a6 = -1.13574198E+05 [K]	   
          NASA a7 = 1.81936795E+01 []	   
        END	   
        UPPER INTERVAL COEFFICIENTS:	   
          NASA a1 = 9.47336526E+00 []	   
          NASA a2 = 3.59407743E-03 [K^-1]	   
          NASA a3 = -1.40334012E-06 [K^-2]	   
          NASA a4 = 2.39113889E-10 [K^-3]	   
          NASA a5 = -1.48513407E-14 [K^-4]	   
          NASA a6 = -1.15816621E+05 [K]	   
          NASA a7 = -2.49736848E+01 []	   
        END	   
      END	   
      REFERENCE STATE:	   
        Option = NASA Format	   
        Reference Pressure = 1 [atm]	   
        Reference Temperature =  145.11 [K]	   
      END      	   
      DYNAMIC VISCOSITY:	   
        Dynamic Viscosity = 0.0000087007 [kg/m/s]	   
        Option = Value	   
      END	   
      REFRACTIVE INDEX:	   
        Option = Value	   
        Refractive Index = 1 [m m^-1]	   
      END	   
      SCATTERING COEFFICIENT:	   
        Option = Value	   
        Scattering Coefficient = 0 [m^-1]	   
      END	   
      ABSORPTION COEFFICIENT:	   
        Absorption Coefficient = 1 [m^-1]	   
        Option = Value	   
      END	   
      THERMAL CONDUCTIVITY:	   
        Option = Value	   
        Thermal Conductivity = 0.0052154 [W m^-1 K^-1]	   
      END	   
      EQUATION OF STATE:	   
        Molar Mass = 88.005 [kg kmol^-1]	   
        Option = Ideal Gas	   
      END	   
    END	   
  END	   

  MATERIAL:CH
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 3.2002020E+00 []
          NASA a2 = 2.0728750E-03 [K^-1]
          NASA a3 = -5.1344310E-06 [K^-2]
          NASA a4 = 5.7338900E-09 [K^-3]
          NASA a5 = -1.9555330E-12 [K^-4]
          NASA a6 = 7.0452590E+04 [K]
          NASA a7 = 3.3315870E+00 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 2.1962230E+00 []
          NASA a2 = 2.3403810E-03 [K^-1]
          NASA a3 = -7.0582010E-07 [K^-2]
          NASA a4 = 9.0075820E-11 [K^-3]
          NASA a5 = -3.8550400E-15 [K^-4]
          NASA a6 = 7.0867230E+04 [K]
          NASA a7 = 9.1783730E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 13.02 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:CH2
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 250 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 4000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 3.7622370E+00 []
          NASA a2 = 1.1598191E-03 [K^-1]
          NASA a3 = 2.4895850E-07 [K^-2]
          NASA a4 = 8.8008360E-10 [K^-3]
          NASA a5 = -7.3324350E-13 [K^-4]
          NASA a6 = 4.5367900E+04 [K]
          NASA a7 = 1.7125770E+00 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 3.6364070E+00 []
          NASA a2 = 1.9330560E-03 [K^-1]
          NASA a3 = -1.6870160E-07 [K^-2]
          NASA a4 = -1.0098994E-10 [K^-3]
          NASA a5 = 1.8082550E-14 [K^-4]
          NASA a6 = 4.5341340E+04 [K]
          NASA a7 = 2.1565600E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 14.03 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:CH2CO
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 2.9749700E+00 []
          NASA a2 = 1.2118712E-02 [K^-1]
          NASA a3 = -2.3450450E-06 [K^-2]
          NASA a4 = -6.4666850E-09 [K^-3]
          NASA a5 = 3.9056490E-12 [K^-4]
          NASA a6 = -7.6326360E+03 [K]
          NASA a7 = 8.6735530E+00 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 6.0388170E+00 []
          NASA a2 = 5.8048400E-03 [K^-1]
          NASA a3 = -1.9209530E-06 [K^-2]
          NASA a4 = 2.7944840E-10 [K^-3]
          NASA a5 = -1.4588676E-14 [K^-4]
          NASA a6 = -8.5834020E+03 [K]
          NASA a7 = -7.6575810E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 42.04 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:CH2O
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 1.6527311E+00 []
          NASA a2 = 1.2631439E-02 [K^-1]
          NASA a3 = -1.8881680E-05 [K^-2]
          NASA a4 = 2.0500310E-08 [K^-3]
          NASA a5 = -8.4132370E-12 [K^-4]
          NASA a6 = -1.4865404E+04 [K]
          NASA a7 = 1.3784820E+01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 2.9956060E+00 []
          NASA a2 = 6.6813210E-03 [K^-1]
          NASA a3 = -2.6289540E-06 [K^-2]
          NASA a4 = 4.7371530E-10 [K^-3]
          NASA a5 = -3.2125170E-14 [K^-4]
          NASA a6 = -1.5320369E+04 [K]
          NASA a7 = 6.9125720E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 30.03 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:CH2OH
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 250 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 4000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 2.8626280E+00 []
          NASA a2 = 1.0015273E-02 [K^-1]
          NASA a3 = -5.2854350E-07 [K^-2]
          NASA a4 = -5.1385390E-09 [K^-3]
          NASA a5 = 2.2460410E-12 [K^-4]
          NASA a6 = -3.3496780E+03 [K]
          NASA a7 = 1.0397938E+01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 6.3275200E+00 []
          NASA a2 = 3.6082700E-03 [K^-1]
          NASA a3 = -3.2015470E-07 [K^-2]
          NASA a4 = -1.9387500E-10 [K^-3]
          NASA a5 = 3.5097040E-14 [K^-4]
          NASA a6 = -4.4745090E+03 [K]
          NASA a7 = -8.3293650E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 31.03 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:CH3
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 2.4304420E+00 []
          NASA a2 = 1.1124099E-02 [K^-1]
          NASA a3 = -1.6802200E-05 [K^-2]
          NASA a4 = 1.6218288E-08 [K^-3]
          NASA a5 = -5.8649520E-12 [K^-4]
          NASA a6 = 1.6423781E+04 [K]
          NASA a7 = 6.7897940E+00 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 2.8440510E+00 []
          NASA a2 = 6.1379740E-03 [K^-1]
          NASA a3 = -2.2303450E-06 [K^-2]
          NASA a4 = 3.7851610E-10 [K^-3]
          NASA a5 = -2.4521590E-14 [K^-4]
          NASA a6 = 1.6437809E+04 [K]
          NASA a7 = 5.4526970E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 15.03 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:CH3CO
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 3.1252780E+00 []
          NASA a2 = 9.7782200E-03 [K^-1]
          NASA a3 = 4.5214480E-06 [K^-2]
          NASA a4 = -9.0094620E-09 [K^-3]
          NASA a5 = 3.1937170E-12 [K^-4]
          NASA a6 = -4.1085070E+03 [K]
          NASA a7 = 1.1228854E+01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 5.6122790E+00 []
          NASA a2 = 8.4498860E-03 [K^-1]
          NASA a3 = -2.8541470E-06 [K^-2]
          NASA a4 = 4.2383760E-10 [K^-3]
          NASA a5 = -2.2684030E-14 [K^-4]
          NASA a6 = -5.1878630E+03 [K]
          NASA a7 = -3.2749490E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 43.05 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:CH3NO2
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1500 [K]
          Upper Temperature = 4000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 3.2247160E-01 []
          NASA a2 = 2.6651460E-02 [K^-1]
          NASA a3 = -1.9305730E-05 [K^-2]
          NASA a4 = 7.7626200E-09 [K^-3]
          NASA a5 = -1.3987461E-12 [K^-4]
          NASA a6 = -9.5975270E+03 [K]
          NASA a7 = 2.7261560E+01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 1.0901579E+01 []
          NASA a2 = 4.3263810E-03 [K^-1]
          NASA a3 = -4.2035470E-07 [K^-2]
          NASA a4 = -1.8930700E-10 [K^-3]
          NASA a5 = 3.4174440E-14 [K^-4]
          NASA a6 = -1.3708618E+04 [K]
          NASA a7 = -3.0731830E+01 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 61.04 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:CH3O
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 3000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 2.1062040E+00 []
          NASA a2 = 7.2165950E-03 [K^-1]
          NASA a3 = 5.3384720E-06 [K^-2]
          NASA a4 = -7.3776360E-09 [K^-3]
          NASA a5 = 2.0756100E-12 [K^-4]
          NASA a6 = 9.7860110E+02 [K]
          NASA a7 = 1.3152177E+01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 3.7707990E+00 []
          NASA a2 = 7.8714970E-03 [K^-1]
          NASA a3 = -2.6563840E-06 [K^-2]
          NASA a4 = 3.9444310E-10 [K^-3]
          NASA a5 = -2.1126160E-14 [K^-4]
          NASA a6 = 1.2783252E+02 [K]
          NASA a7 = 2.9295750E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 31.03 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:CH3OH
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 2.6601150E+00 []
          NASA a2 = 7.3415080E-03 [K^-1]
          NASA a3 = 7.1700500E-06 [K^-2]
          NASA a4 = -8.7931940E-09 [K^-3]
          NASA a5 = 2.3905700E-12 [K^-4]
          NASA a6 = -2.5353480E+04 [K]
          NASA a7 = 1.1232631E+01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 4.0290610E+00 []
          NASA a2 = 9.3765930E-03 [K^-1]
          NASA a3 = -3.0502540E-06 [K^-2]
          NASA a4 = 4.3587930E-10 [K^-3]
          NASA a5 = -2.2247230E-14 [K^-4]
          NASA a6 = -2.6157910E+04 [K]
          NASA a7 = 2.3781950E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 32.04 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:CH4
    Material Description = Methane CH4 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.07787415E+01 []
          NASA a2 = 0.01747668E+00 [K^-1]
          NASA a3 = -0.02783409E-03 [K^-2]
          NASA a4 = 0.03049708E-06 [K^-3]
          NASA a5 = -0.01223931E-09 [K^-4]
          NASA a6 = -0.09825229E+05 [K]
          NASA a7 = 0.01372219E+03 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.01683479E+02 []
          NASA a2 = 0.01023724E+00 [K^-1]
          NASA a3 = -0.03875129E-04 [K^-2]
          NASA a4 = 0.06785585E-08 [K^-3]
          NASA a5 = -0.04503423E-12 [K^-4]
          NASA a6 = -0.01008079E+06 [K]
          NASA a7 = 0.09623395E+02 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 11.1E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 343E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 16.04 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:CN
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 3.6632040E+00 []
          NASA a2 = -1.1565290E-03 [K^-1]
          NASA a3 = 2.1634090E-06 [K^-2]
          NASA a4 = 1.8542080E-10 [K^-3]
          NASA a5 = -8.2146950E-13 [K^-4]
          NASA a6 = 5.1281180E+04 [K]
          NASA a7 = 3.7390150E+00 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 3.7201190E+00 []
          NASA a2 = 1.5183506E-04 [K^-1]
          NASA a3 = 1.9873810E-07 [K^-2]
          NASA a4 = -3.7983710E-11 [K^-3]
          NASA a5 = 1.3282296E-15 [K^-4]
          NASA a6 = 5.1116260E+04 [K]
          NASA a7 = 2.8885970E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 26.02 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:C2H
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 3.0506670E+00 []
          NASA a2 = 6.0516740E-03 [K^-1]
          NASA a3 = -4.9566340E-06 [K^-2]
          NASA a4 = 2.8041590E-09 [K^-3]
          NASA a5 = -8.1933320E-13 [K^-4]
          NASA a6 = 6.6300110E+04 [K]
          NASA a7 = 5.9543610E+00 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 4.4276880E+00 []
          NASA a2 = 2.2162680E-03 [K^-1]
          NASA a3 = -6.0489520E-07 [K^-2]
          NASA a4 = 9.8825170E-11 [K^-3]
          NASA a5 = -7.3511790E-15 [K^-4]
          NASA a6 = 6.5904150E+04 [K]
          NASA a7 = -1.1994418E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 25.03 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:C2H2
    Material Description = Acetylene C2H2 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.02013562E+02 []
          NASA a2 = 0.01519045E+00 [K^-1]
          NASA a3 = -0.01616319E-03 [K^-2]
          NASA a4 = 0.09078992E-07 [K^-3]
          NASA a5 = -0.01912746E-10 [K^-4]
          NASA a6 = 0.02612444E+06 [K]
          NASA a7 = 0.08805378E+02 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.04436770E+02 []
          NASA a2 = 0.05376039E-01 [K^-1]
          NASA a3 = -0.01912817E-04 [K^-2]
          NASA a4 = 0.03286379E-08 [K^-3]
          NASA a5 = -0.02156710E-12 [K^-4]
          NASA a6 = 0.02566766E+06 [K]
          NASA a7 = -0.02800338E+02 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 1.788E-05 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 2.59E-02 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 26.04 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:C2H3
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 2.4592760E+00 []
          NASA a2 = 7.3714760E-03 [K^-1]
          NASA a3 = 2.1098720E-06 [K^-2]
          NASA a4 = -1.3216421E-09 [K^-3]
          NASA a5 = -1.1847838E-12 [K^-4]
          NASA a6 = 3.3352250E+04 [K]
          NASA a7 = 1.1556202E+01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 5.9334680E+00 []
          NASA a2 = 4.0177450E-03 [K^-1]
          NASA a3 = -3.9667390E-07 [K^-2]
          NASA a4 = -1.4412666E-10 [K^-3]
          NASA a5 = 2.3786430E-14 [K^-4]
          NASA a6 = 3.1854340E+04 [K]
          NASA a7 = -8.5303130E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 27.05 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:C2H4
    Material Description = Ethene C2H4 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = -0.08614880E+01 []
          NASA a2 = 0.02796163E+00 [K^-1]
          NASA a3 = -0.03388677E-03 [K^-2]
          NASA a4 = 0.02785152E-06 [K^-3]
          NASA a5 = -0.09737879E-10 [K^-4]
          NASA a6 = 0.05573046E+05 [K]
          NASA a7 = 0.02421149E+03 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.03528419E+02 []
          NASA a2 = 0.01148518E+00 [K^-1]
          NASA a3 = -0.04418385E-04 [K^-2]
          NASA a4 = 0.07844601E-08 [K^-3]
          NASA a5 = -0.05266848E-12 [K^-4]
          NASA a6 = 0.04428289E+05 [K]
          NASA a7 = 0.02230389E+02 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 1.027E-05 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 2.05E-02 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 28.05 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:C2H5
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 2.6907010E+00 []
          NASA a2 = 8.7191330E-03 [K^-1]
          NASA a3 = 4.4198380E-06 [K^-2]
          NASA a4 = 9.3387030E-10 [K^-3]
          NASA a5 = -3.9277730E-12 [K^-4]
          NASA a6 = 1.2870404E+04 [K]
          NASA a7 = 1.2138195E+01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 7.1904800E+00 []
          NASA a2 = 6.4840770E-03 [K^-1]
          NASA a3 = -6.4280640E-07 [K^-2]
          NASA a4 = -2.3478790E-10 [K^-3]
          NASA a5 = 3.8808770E-14 [K^-4]
          NASA a6 = 1.0674549E+04 [K]
          NASA a7 = -1.4780892E+01 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 29.06 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:C2H6
    Material Description = Ethane C2H6 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 4000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.01462539E+02 []
          NASA a2 = 0.01549467E+00 [K^-1]
          NASA a3 = 0.05780507E-04 [K^-2]
          NASA a4 = -0.01257832E-06 [K^-3]
          NASA a5 = 0.04586267E-10 [K^-4]
          NASA a6 = -0.01123918E+06 [K]
          NASA a7 = 0.01443229E+03 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.04825938E+02 []
          NASA a2 = 0.01384043E+00 [K^-1]
          NASA a3 = -0.04557259E-04 [K^-2]
          NASA a4 = 0.06724967E-08 [K^-3]
          NASA a5 = -0.03598161E-12 [K^-4]
          NASA a6 = -0.01271779E+06 [K]
          NASA a7 = -0.05239507E+02 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.929E-05 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 2.06E-02 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 30.07 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL: C2H6O	   
    Material Description = Ethanol C2H6O
    Option = Pure Substance	   
    Thermodynamic State = Gas	   
    Material Group = Gas Phase Combustion	   
    PROPERTIES:	   
      Option = General Material	   
      SPECIFIC HEAT CAPACITY:	   
        Option = NASA Format	   
        TEMPERATURE LIMITS:	   
          Lower Temperature = 200 [K]	   
          Midpoint Temperature = 1000 [K]	   
          Upper Temperature = 6000 [K]	   
        END	   
        LOWER INTERVAL COEFFICIENTS:	   
          NASA a1 = 0.48586957E+01 []	   
          NASA a2 = -0.37401726E-02 [K^-1]	   
          NASA a3 = 0.69555378E-04 [K^-2]	   
          NASA a4 = -0.88654796E-07 [K^-3]	   
          NASA a5 = 0.35168835E-10 [K^-4]	   
          NASA a6 = -0.29996132E+05 [K]	   
          NASA a7 = 0.48018545E+01 []	   
        END	   
        UPPER INTERVAL COEFFICIENTS:	   
          NASA a1 = 0.65624365E+01 []	   
          NASA a2 = 0.15204222E-01 [K^-1]	   
          NASA a3 = -0.53896795E-05 [K^-2]	   
          NASA a4 = 0.86225011E-09 [K^-3]	   
          NASA a5 = -0.51289787E-13 [K^-4]	   
          NASA a6 = -0.31525621E+05 [K]	   
          NASA a7 = -0.94730202E+01 []	   
        END	   
      END	   
      REFERENCE STATE:	   
        Option = NASA Format	   
        Reference Pressure = 1 [atm]	   
        Reference Temperature =  298.15 [K]	   
      END      	   
      DYNAMIC VISCOSITY:	   
        Dynamic Viscosity = 0.00001576 [kg/m/s]	   
        Option = Value	   
      END	   
      REFRACTIVE INDEX:	   
        Option = Value	   
        Refractive Index = 1 [m m^-1]	   
      END	   
      SCATTERING COEFFICIENT:	   
        Option = Value	   
        Scattering Coefficient = 0 [m^-1]	   
      END	   
      ABSORPTION COEFFICIENT:	   
        Absorption Coefficient = 1 [m^-1]	   
        Option = Value	   
      END	   
      THERMAL CONDUCTIVITY:	   
        Option = Value	   
        Thermal Conductivity = 0.034559 [W m^-1 K^-1]	   
      END	   
      EQUATION OF STATE:	   
        Molar Mass = 46.069 [kg kmol^-1]	   
        Option = Ideal Gas	   
      END	   
    END	   
  END	 

  MATERIAL:C3H4
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = -2.1319680E-01 []
          NASA a2 = 3.3587130E-02 [K^-1]
          NASA a3 = -3.8048700E-05 [K^-2]
          NASA a4 = 2.7458380E-08 [K^-3]
          NASA a5 = -8.6900440E-12 [K^-4]
          NASA a6 = 2.1620480E+04 [K]
          NASA a7 = 2.0293920E+01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 5.7291440E+00 []
          NASA a2 = 1.2368045E-02 [K^-1]
          NASA a3 = -4.8056260E-06 [K^-2]
          NASA a4 = 8.6013640E-10 [K^-3]
          NASA a5 = -5.8128020E-14 [K^-4]
          NASA a6 = 2.0129840E+04 [K]
          NASA a7 = -9.4486680E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 40.06 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:C3H6
    Material Description = Propene C3H6 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.01493307E+02 []
          NASA a2 = 0.02092518E+00 [K^-1]
          NASA a3 = 0.04486794E-04 [K^-2]
          NASA a4 = -0.01668912E-06 [K^-3]
          NASA a5 = 0.07158146E-10 [K^-4]
          NASA a6 = 0.01074826E+05 [K]
          NASA a7 = 0.01614534E+03 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.06732257E+02 []
          NASA a2 = 0.01490834E+00 [K^-1]
          NASA a3 = -0.04949899E-04 [K^-2]
          NASA a4 = 0.07212022E-08 [K^-3]
          NASA a5 = -0.03766204E-12 [K^-4]
          NASA a6 = -0.09235703E+04 [K]
          NASA a7 = -0.01331335E+03 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 1.788E-05 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 2.59E-02 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 42.08 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:C3H6O	   
    Material Description = Acetone Vapour (C3H6O)	   
    Option = Pure Substance	   
    Thermodynamic State = Gas	   
    Material Group = Gas Phase Combustion	   
    PROPERTIES:	   
      Option = General Material	   
      SPECIFIC HEAT CAPACITY:	   
        Option = NASA Format	   
        TEMPERATURE LIMITS:	   
          Lower Temperature = 200 [K]	   
          Midpoint Temperature = 1000 [K]	   
          Upper Temperature = 6000 [K]	   
        END	   
        LOWER INTERVAL COEFFICIENTS:	   
          NASA a1 = 5.55638920E+00 []	   
          NASA a2 = -2.83863547E-03 [K^-1]	   
          NASA a3 = 7.05722951E-05 [K^-2]	   
          NASA a4 = -8.78130984E-08 [K^-3]	   
          NASA a5 = 3.40290951E-11 [K^-4]	   
          NASA a6 = -2.78325393E+04 [K]	   
          NASA a7 = 2.31960221E+00 []	   
        END	   
        UPPER INTERVAL COEFFICIENTS:	   
          NASA a1 = 7.29796974E+00 []	   
          NASA a2 = 1.75656913E-02 [K^-1]	   
          NASA a3 = -6.31678065E-06 [K^-2]	   
          NASA a4 = 1.02025553E-09 [K^-3]	   
          NASA a5 = -6.10903592E-14 [K^-4]	   
          NASA a6 = -2.95368927E+04 [K]	   
          NASA a7 = -1.27591704E+01 []	   
        END	   
      END	   
      REFERENCE STATE:	   
        Option = NASA Format	   
        Reference Pressure = 1 [atm]	   
        Reference Temperature =  298.15 [K]	   
      END      	   
      DYNAMIC VISCOSITY:	   
        Dynamic Viscosity = 0.000015238 [kg/m/s]	   
        Option = Value	   
      END	   
      REFRACTIVE INDEX:	   
        Option = Value	   
        Refractive Index = 1 [m m^-1]	   
      END	   
      SCATTERING COEFFICIENT:	   
        Option = Value	   
        Scattering Coefficient = 0 [m^-1]	   
      END	   
      ABSORPTION COEFFICIENT:	   
        Absorption Coefficient = 1 [m^-1]	   
        Option = Value	   
      END	   
      THERMAL CONDUCTIVITY:	   
        Option = Value	   
        Thermal Conductivity = 0.027829 [W m^-1 K^-1]	   
      END	   
      EQUATION OF STATE:	   
        Molar Mass = 58.08 [kg kmol^-1]	   
        Option = Ideal Gas	   
      END	   
    END	   
  END	   

  MATERIAL:I C3H7
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 1.7132990E+00 []
          NASA a2 = 2.5426160E-02 [K^-1]
          NASA a3 = 1.5808083E-06 [K^-2]
          NASA a4 = -1.8212860E-08 [K^-3]
          NASA a5 = 8.8277100E-12 [K^-4]
          NASA a6 = 7.5358080E+03 [K]
          NASA a7 = 1.2979008E+01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 8.0633690E+00 []
          NASA a2 = 1.5744876E-02 [K^-1]
          NASA a3 = -5.1823910E-06 [K^-2]
          NASA a4 = 7.4772450E-10 [K^-3]
          NASA a5 = -3.8544220E-14 [K^-4]
          NASA a6 = 5.3138710E+03 [K]
          NASA a7 = -2.1926460E+01 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 43.09 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:N C3H7
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 1.9225360E+00 []
          NASA a2 = 2.4789270E-02 [K^-1]
          NASA a3 = 1.8102490E-06 [K^-2]
          NASA a4 = -1.7832650E-08 [K^-3]
          NASA a5 = 8.5829960E-12 [K^-4]
          NASA a6 = 9.7132810E+03 [K]
          NASA a7 = 1.3992715E+01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 7.9782900E+00 []
          NASA a2 = 1.5761134E-02 [K^-1]
          NASA a3 = -5.1732430E-06 [K^-2]
          NASA a4 = 7.4438920E-10 [K^-3]
          NASA a5 = -3.8249780E-14 [K^-4]
          NASA a6 = 7.5794020E+03 [K]
          NASA a7 = -1.9356110E+01 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 43.09 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:C3H8
    Material Description = Propane C3H8 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.08969208E+01 []
          NASA a2 = 0.02668986E+00 [K^-1]
          NASA a3 = 0.05431425E-04 [K^-2]
          NASA a4 = -0.02126001E-06 [K^-3]
          NASA a5 = 0.09243330E-10 [K^-4]
          NASA a6 = -0.01395492E+06 [K]
          NASA a7 = 0.01935533E+03 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.07525217E+02 []
          NASA a2 = 0.01889034E+00 [K^-1]
          NASA a3 = -0.06283924E-04 [K^-2]
          NASA a4 = 0.09179373E-08 [K^-3]
          NASA a5 = -0.04812410E-12 [K^-4]
          NASA a6 = -0.01646455E+06 [K]
          NASA a7 = -0.01784390E+03 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.811E-05 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 1.73E-02 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 44.10 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:C4H2
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 4.0051910E+00 []
          NASA a2 = 1.9810000E-02 [K^-1]
          NASA a3 = -9.8658770E-06 [K^-2]
          NASA a4 = -6.6351580E-09 [K^-3]
          NASA a5 = 6.0774130E-12 [K^-4]
          NASA a6 = 5.4240650E+04 [K]
          NASA a7 = 1.8457360E+00 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 9.0314070E+00 []
          NASA a2 = 6.0472520E-03 [K^-1]
          NASA a3 = -1.9487880E-06 [K^-2]
          NASA a4 = 2.7548630E-10 [K^-3]
          NASA a5 = -1.3856080E-14 [K^-4]
          NASA a6 = 5.2947350E+04 [K]
          NASA a7 = -2.3850670E+01 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 50.06 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:C4H6
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 3.1971080E+00 []
          NASA a2 = 2.0255910E-02 [K^-1]
          NASA a3 = 6.5101920E-06 [K^-2]
          NASA a4 = -1.6584423E-08 [K^-3]
          NASA a5 = 6.4002820E-12 [K^-4]
          NASA a6 = 1.5715203E+04 [K]
          NASA a7 = 9.8956600E+00 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 8.0465830E+00 []
          NASA a2 = 1.6485251E-02 [K^-1]
          NASA a3 = -5.5222270E-06 [K^-2]
          NASA a4 = 8.1235930E-10 [K^-3]
          NASA a5 = -4.2950780E-14 [K^-4]
          NASA a6 = 1.3701305E+04 [K]
          NASA a7 = -1.8004570E+01 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 54.09 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:C4H8
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 1.1811380E+00 []
          NASA a2 = 3.0853380E-02 [K^-1]
          NASA a3 = 5.0865240E-06 [K^-2]
          NASA a4 = -2.4654880E-08 [K^-3]
          NASA a5 = 1.1110192E-11 [K^-4]
          NASA a6 = -1.7904000E+03 [K]
          NASA a7 = 2.1062470E+01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 2.0535840E+00 []
          NASA a2 = 3.4350500E-02 [K^-1]
          NASA a3 = -1.5883196E-05 [K^-2]
          NASA a4 = 3.3089660E-09 [K^-3]
          NASA a5 = -2.5361040E-13 [K^-4]
          NASA a6 = -2.1397230E+03 [K]
          NASA a7 = 1.5543201E+01 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 56.11 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:C4H10
    Material Description = Butane C4H10 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1500 [K]
          Upper Temperature = 4000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = -0.02256618E+02 []
          NASA a2 = 0.05881732E+00 [K^-1]
          NASA a3 = -0.04525783E-03 [K^-2]
          NASA a4 = 0.02037115E-06 [K^-3]
          NASA a5 = -0.04079458E-10 [K^-4]
          NASA a6 = -0.01760233E+06 [K]
          NASA a7 = 0.03329595E+03 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.01998785E+03 []
          NASA a2 = 0.01037281E+00 [K^-1]
          NASA a3 = -0.09610818E-05 [K^-2]
          NASA a4 = -0.04623018E-08 [K^-3]
          NASA a5 = 0.08202828E-12 [K^-4]
          NASA a6 = -0.02625571E+06 [K]
          NASA a7 = -0.08837907E+03 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 7.5425E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 162.298E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 58.12 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:I C4H10	   
    Material Description = Isobutane Vapour (C4H10)	   
    Option = Pure Substance	   
    Thermodynamic State = Gas	   
    Material Group = Gas Phase Combustion	   
    PROPERTIES:	   
      Option = General Material	   
      SPECIFIC HEAT CAPACITY:	   
        Option = NASA Format	   
        TEMPERATURE LIMITS:	   
          Lower Temperature = 200 [K]	   
          Midpoint Temperature = 1000 [K]	   
          Upper Temperature = 6000 [K]	   
        END	   
        LOWER INTERVAL COEFFICIENTS:	   
          NASA a1 = 4.45479140E+00 []	   
          NASA a2 = 8.26058864E-03 [K^-1]	   
          NASA a3 = 8.29886433E-05 [K^-2]	   
          NASA a4 = -1.14647616E-07 [K^-3]	   
          NASA a5 = 4.64569994E-11 [K^-4]	   
          NASA a6 = -1.84593929E+04 [K]	   
          NASA a7 = 4.92740653E+00 []	   
        END	   
        UPPER INTERVAL COEFFICIENTS:	   
          NASA a1 = 9.76991697E+00 []	   
          NASA a2 = 2.54997141E-02 [K^-1]	   
          NASA a3 = -9.14142587E-06 [K^-2]	   
          NASA a4 = 1.47328201E-09 [K^-3]	   
          NASA a5 = -8.80799697E-14 [K^-4]	   
          NASA a6 = -2.14052667E+04 [K]	   
          NASA a7 = -3.00329670E+01 []	   
        END	   
      END	   
      REFERENCE STATE:	   
        Option = NASA Format	   
        Reference Pressure = 1 [atm]	   
        Reference Temperature =  261.34 [K]	   
      END      	   
      DYNAMIC VISCOSITY:	   
        Dynamic Viscosity = 0.0000065811 [kg/m/s]	   
        Option = Value	   
      END	   
      REFRACTIVE INDEX:	   
        Option = Value	   
        Refractive Index = 1 [m m^-1]	   
      END	   
      SCATTERING COEFFICIENT:	   
        Option = Value	   
        Scattering Coefficient = 0 [m^-1]	   
      END	   
      ABSORPTION COEFFICIENT:	   
        Absorption Coefficient = 1 [m^-1]	   
        Option = Value	   
      END	   
      THERMAL CONDUCTIVITY:	   
        Option = Value	   
        Thermal Conductivity = 0.013209 [W m^-1 K^-1]	   
      END	   
      EQUATION OF STATE:	   
        Molar Mass = 58.123 [kg kmol^-1]	   
        Option = Ideal Gas	   
      END	   
    END	   
  END	   

  MATERIAL:C5H12
    Material Description = Pentane C5H12 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 4000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.01877908E+02 []
          NASA a2 = 0.04121646E+00 [K^-1]
          NASA a3 = 0.01253234E-03 [K^-2]
          NASA a4 = -0.03701537E-06 [K^-3]
          NASA a5 = 0.01525569E-09 [K^-4]
          NASA a6 = -0.02003816E+06 [K]
          NASA a7 = 0.01877257E+03 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.01667798E+03 []
          NASA a2 = 0.02114483E+00 [K^-1]
          NASA a3 = -0.03533321E-04 [K^-2]
          NASA a4 = -0.05742202E-08 [K^-3]
          NASA a5 = 0.01515948E-11 [K^-4]
          NASA a6 = -0.02553670E+06 [K]
          NASA a7 = -0.06372940E+03 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 6.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 14.4E-03 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 72.15 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:C6H6
    Material Description = Benzene C6H6 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = -0.03138012E+02 []
          NASA a2 = 0.04723103E+00 [K^-1]
          NASA a3 = -0.02962208E-04 [K^-2]
          NASA a4 = -0.03262819E-06 [K^-3]
          NASA a5 = 0.01718692E-09 [K^-4]
          NASA a6 = 0.08890031E+05 [K]
          NASA a7 = 0.03657573E+03 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.01291074E+03 []
          NASA a2 = 0.01723297E+00 [K^-1]
          NASA a3 = -0.05024211E-04 [K^-2]
          NASA a4 = 0.05893497E-08 [K^-3]
          NASA a5 = -0.01947521E-12 [K^-4]
          NASA a6 = 0.03664512E+05 [K]
          NASA a7 = -0.05002699E+03 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 7.5684E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 99.6722E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 78.11 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:C6H5OH	   
    Material Description = Phenol Vapour (C6H6O)	   
    Option = Pure Substance	   
    Thermodynamic State = Gas	   
    Material Group = Gas Phase Combustion	   
    PROPERTIES:	   
      Option = General Material	   
      SPECIFIC HEAT CAPACITY:	   
        Option = NASA Format	   
        TEMPERATURE LIMITS:	   
          Lower Temperature = 200 [K]	   
          Midpoint Temperature = 1000 [K]	   
          Upper Temperature = 6000 [K]	   
        END	   
        LOWER INTERVAL COEFFICIENTS:	   
          NASA a1 = -2.90978575E-01 []	   
          NASA a2 = 4.08562397E-02 [K^-1]	   
          NASA a3 = 2.42829425E-05 [K^-2]	   
          NASA a4 = -7.14477617E-08 [K^-3]	   
          NASA a5 = 3.46002146E-11 [K^-4]	   
          NASA a6 = -1.34129780E+04 [K]	   
          NASA a7 = 2.68745637E+01 []	   
        END	   
        UPPER INTERVAL COEFFICIENTS:	   
          NASA a1 = 1.41552427E+01 []	   
          NASA a2 = 1.99350340E-02 [K^-1]	   
          NASA a3 = -7.18219540E-06 [K^-2]	   
          NASA a4 = 1.16229002E-09 [K^-3]	   
          NASA a5 = -6.97147483E-14 [K^-4]	   
          NASA a6 = -1.81287441E+04 [K]	   
          NASA a7 = -5.17984911E+01 []	   
        END	   
      END	   
      REFERENCE STATE:	   
        Option = NASA Format	   
        Reference Pressure = 1 [atm]	   
        Reference Temperature =  298.15 [K]	   
      END      	   
      DYNAMIC VISCOSITY:	   
        Dynamic Viscosity = 0.00001825 [kg/m/s]	   
        Option = Value	     
      END	   
      REFRACTIVE INDEX:	   
        Option = Value	   
        Refractive Index = 1 [m m^-1]	   
      END	   
      SCATTERING COEFFICIENT:	   
        Option = Value	   
        Scattering Coefficient = 0 [m^-1]	   
      END	   
      ABSORPTION COEFFICIENT:	   
        Absorption Coefficient = 1 [m^-1]	   
        Option = Value	   
      END	   
      THERMAL CONDUCTIVITY:	   
        Option = Value	   
        Thermal Conductivity = 0.027831 [W m^-1 K^-1]	   
      END	   
      EQUATION OF STATE:	   
        Molar Mass = 94.113 [kg kmol^-1]	   
        Option = Ideal Gas	   
      END	   
    END	   
  END	   

  MATERIAL:C6H12	   
    Material Description = Cyclohexane Vapour (C6H12)	   
    Option = Pure Substance	   
    Thermodynamic State = Gas	   
    Material Group = Gas Phase Combustion	   
    PROPERTIES:	   
      Option = General Material	   
      SPECIFIC HEAT CAPACITY:	   
        Option = NASA Format	   
        TEMPERATURE LIMITS:	   
          Lower Temperature = 200 [K]	   
          Midpoint Temperature = 1000 [K]	   
          Upper Temperature = 6000 [K]	   
        END	   
        LOWER INTERVAL COEFFICIENTS:	   
          NASA a1 = 4.04357527E+00 []	   
          NASA a2 = -6.19608335E-03 [K^-1]	   
          NASA a3 = 1.76622274E-04 [K^-2]	   
          NASA a4 = -2.22968474E-07 [K^-3]	   
          NASA a5 = 8.63668578E-11 [K^-4]	   
          NASA a6 = -1.69203544E+04 [K]	   
          NASA a7 = 8.52527441E+00 []	   
        END	   
        UPPER INTERVAL COEFFICIENTS:	   
          NASA a1 = 1.32145970E+01 []	   
          NASA a2 = 3.58243434E-02 [K^-1]	   
          NASA a3 = -1.32110852E-05 [K^-2]	   
          NASA a4 = 2.17202521E-09 [K^-3]	   
          NASA a5 = -1.31730622E-13 [K^-4]	   
          NASA a6 = -2.28092102E+04 [K]	   
          NASA a7 = -5.53518322E+01 []	   
        END	   
      END	   
      REFERENCE STATE:	   
        Option = NASA Format	   
        Reference Pressure = 1 [atm]	   
        Reference Temperature =  298.15 [K]	   
      END      	   
      DYNAMIC VISCOSITY:	   
        Dynamic Viscosity = 0.0005395 [kg/m/s]	   
        Option = Value	   
      END	   
      REFRACTIVE INDEX:	   
        Option = Value	   
        Refractive Index = 1 [m m^-1]	   
      END	   
      SCATTERING COEFFICIENT:	   
        Option = Value	   
        Scattering Coefficient = 0 [m^-1]	   
      END	   
      ABSORPTION COEFFICIENT:	   
        Absorption Coefficient = 1 [m^-1]	   
        Option = Value	   
      END	   
      THERMAL CONDUCTIVITY:	   
        Option = Value	   
        Thermal Conductivity = 0.1228 [W m^-1 K^-1]	   
      END	   
      EQUATION OF STATE:	   
        Molar Mass = 84.161 [kg kmol^-1]	   
        Option = Ideal Gas	   
      END	   
    END	   
  END	   

  MATERIAL:C6H14
    Material Description = Hexane C6H14 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 4000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.01836174E+02 []
          NASA a2 = 0.05098461E+00 [K^-1]
          NASA a3 = 0.01259586E-03 [K^-2]
          NASA a4 = -0.04428362E-06 [K^-3]
          NASA a5 = 0.01872237E-09 [K^-4]
          NASA a6 = -0.02292750E+06 [K]
          NASA a7 = 0.02088145E+03 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.02280472E+03 []
          NASA a2 = 0.02097989E+00 [K^-1]
          NASA a3 = -0.03530674E-04 [K^-2]
          NASA a4 = -0.05466245E-08 [K^-3]
          NASA a5 = 0.01478950E-11 [K^-4]
          NASA a6 = -0.03073757E+06 [K]
          NASA a7 = -0.09583162E+03 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 6.1E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 13.8E-03 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 86.178 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:I C6H14	   
    Material Description = Isohexane (2-Methylpentane) Vapour (C6H14)	   
    Option = Pure Substance	   
    Thermodynamic State = Gas	   
    Material Group = Gas Phase Combustion	   
    PROPERTIES:	   
      Option = General Material	   
      SPECIFIC HEAT CAPACITY:	   
        Option = NASA Format	   
        TEMPERATURE LIMITS:	   
          Lower Temperature = 298.15 [K]	   
          Midpoint Temperature = 1000 [K]	   
          Upper Temperature = 5000 [K]	   
        END	   
        LOWER INTERVAL COEFFICIENTS:	   
          NASA a1 = -0.18831303E+00 []	   
          NASA a2 = 0.62825959E-01 [K^-1]	   
          NASA a3 = -0.96052544E-05 [K^-2]	   
          NASA a4 = -0.26183767E-07 [K^-3]	   
          NASA a5 = 0.13717321E-10 [K^-4]	   
          NASA a6 = -0.23599561E+05 [K]	   
          NASA a7 = 0.28793617E+02 []	   
        END	   
        UPPER INTERVAL COEFFICIENTS:	   
          NASA a1 = 0.13108042E+02 []	   
          NASA a2 = 0.39278025E-01 [K^-1]	   
          NASA a3 = -0.14080404E-04 [K^-2]	   
          NASA a4 = 0.24208876E-08 [K^-3]	   
          NASA a5 = -0.16060487E-12 [K^-4]	   
          NASA a6 = -0.28005811E+05 [K]	   
          NASA a7 = -0.43334246E+02 []	   
        END	   
      END	   
      REFERENCE STATE:	   
        Option = NASA Format	   
        Reference Pressure = 1 [atm]	   
        Reference Temperature =  298.15 [K]	   
      END      	   
      DYNAMIC VISCOSITY:	   
        Dynamic Viscosity = 0.000012759 [kg/m/s]	   
        Option = Value	   
      END	   
      REFRACTIVE INDEX:	   
        Option = Value	   
        Refractive Index = 1 [m m^-1]	   
      END	   
      SCATTERING COEFFICIENT:	   
        Option = Value	   
        Scattering Coefficient = 0 [m^-1]	   
      END	   
      ABSORPTION COEFFICIENT:	   
        Absorption Coefficient = 1 [m^-1]	   
        Option = Value	   
      END	   
      THERMAL CONDUCTIVITY:	   
        Option = Value	   
        Thermal Conductivity = 0.028958 [W m^-1 K^-1]	   
      END	   
      EQUATION OF STATE:	   
        Molar Mass = 86.177 [kg kmol^-1]	   
        Option = Ideal Gas	   
      END	   
    END	   
  END	   

  MATERIAL:C7H8	   
    Material Description = Toluene Vapour (C7H8)	   
    Option = Pure Substance	   
    Thermodynamic State = Gas	   
    Material Group = Gas Phase Combustion	   
    PROPERTIES:	   
      Option = General Material	   
      SPECIFIC HEAT CAPACITY:	   
        Option = NASA Format	   
        TEMPERATURE LIMITS:	   
          Lower Temperature = 200 [K]	   
          Midpoint Temperature = 1000 [K]	   
          Upper Temperature = 6000 [K]	   
        END	   
        LOWER INTERVAL COEFFICIENTS:	   
          NASA a1 = 1.61200102E+00 []	   
          NASA a2 = 2.11179855E-02 [K^-1]	   
          NASA a3 = 8.53239986E-05 [K^-2]	   
          NASA a4 = -1.32568501E-07 [K^-3]	   
          NASA a5 = 5.59411406E-11 [K^-4]	   
          NASA a6 = 4.09654820E+03 [K]	   
          NASA a7 = 2.02969771E+01 []	   
        END	   
        UPPER INTERVAL COEFFICIENTS:	   
          NASA a1 = 1.29393610E+01 []	   
          NASA a2 = 2.66922277E-02 [K^-1]	   
          NASA a3 = -9.68422041E-06 [K^-2]	   
          NASA a4 = 1.57392386E-09 [K^-3]	   
          NASA a5 = -9.46671699E-14 [K^-4]	   
          NASA a6 = -6.76971149E+02 [K]	   
          NASA a7 = -4.67249759E+01 []	   
        END	   
      END	   
      REFERENCE STATE:	   
        Option = NASA Format	   
        Reference Pressure = 1 [atm]	   
        Reference Temperature =  298.15 [K]	   
      END      	   
      DYNAMIC VISCOSITY:	   
        Dynamic Viscosity = 0.00085978 [kg/m/s]	   
        Option = Value	   
      END	   
      REFRACTIVE INDEX:	   
        Option = Value	   
        Refractive Index = 1 [m m^-1]	   
      END	   
      SCATTERING COEFFICIENT:	   
        Option = Value	   
        Scattering Coefficient = 0 [m^-1]	   
      END	   
      ABSORPTION COEFFICIENT:	   
        Absorption Coefficient = 1 [m^-1]	   
        Option = Value	   
      END	   
      THERMAL CONDUCTIVITY:	   
        Option = Value	   
        Thermal Conductivity = 0.12987 [W m^-1 K^-1]	   
      END	   
      EQUATION OF STATE:	   
        Molar Mass = 92.141 [kg kmol^-1]	   
        Option = Ideal Gas	   
      END	   
    END	   
  END	   
	   
  MATERIAL:C7H16	   
    Material Description = Heptane Vapour (C7H16)	   
    Option = Pure Substance	   
    Thermodynamic State = Gas	   
    Material Group = Gas Phase Combustion	   
    PROPERTIES:	   
      Option = General Material	   
      SPECIFIC HEAT CAPACITY:	   
        Option = NASA Format	   
        TEMPERATURE LIMITS:	   
          Lower Temperature = 200 [K]	   
          Midpoint Temperature = 1000 [K]	   
          Upper Temperature = 6000 [K]	   
        END	   
        LOWER INTERVAL COEFFICIENTS:	   
          NASA a1 = 1.11532994E+01 []	   
          NASA a2 = -9.49419773E-03 [K^-1]	   
          NASA a3 = 1.95572075E-04 [K^-2]	   
          NASA a4 = -2.49753662E-07 [K^-3]	   
          NASA a5 = 9.84877715E-11 [K^-4]	   
          NASA a6 = -2.67688904E+04 [K]	   
          NASA a7 = -1.59096837E+01 []	   
        END	   
        UPPER INTERVAL COEFFICIENTS:	   
          NASA a1 = 2.04565203E+01 []	   
          NASA a2 = 3.48575357E-02 [K^-1]	   
          NASA a3 = -1.09226846E-05 [K^-2]	   
          NASA a4 = 1.67201776E-09 [K^-3]	   
          NASA a5 = -9.81024850E-14 [K^-4]	   
          NASA a6 = -3.25556365E+04 [K]	   
          NASA a7 = -8.04405017E+01 []	   
        END	   
      END	   
      REFERENCE STATE:	   
        Option = NASA Format	   
        Reference Pressure = 1 [atm]	   
        Reference Temperature =  298.15 [K]	   
      END      	   
      DYNAMIC VISCOSITY:	   
        Dynamic Viscosity = 0.00038849 [kg/m/s]	   
        Option = Value	   
      END	   
      REFRACTIVE INDEX:	   
        Option = Value	   
        Refractive Index = 1 [m m^-1]	   
      END	   
      SCATTERING COEFFICIENT:	   
        Option = Value	   
        Scattering Coefficient = 0 [m^-1]	   
      END	   
      ABSORPTION COEFFICIENT:	   
        Absorption Coefficient = 1 [m^-1]	   
        Option = Value	   
      END	   
      THERMAL CONDUCTIVITY:	   
        Option = Value	   
        Thermal Conductivity = 0.13125 [W m^-1 K^-1]	   
      END	   
      EQUATION OF STATE:	   
        Molar Mass = 100.204 [kg kmol^-1]	   
        Option = Ideal Gas	   
      END	   
    END	   
  END	   
	   
  MATERIAL:C8H18	   
    Material Description = N-Octane Vapour (C8H18)	   
    Option = Pure Substance	   
    Thermodynamic State = Gas	   
    Material Group = Gas Phase Combustion	   
    PROPERTIES:	   
      Option = General Material	   
      SPECIFIC HEAT CAPACITY:	   
        Option = NASA Format	   
        TEMPERATURE LIMITS:	   
          Lower Temperature = 200 [K]	   
          Midpoint Temperature = 1000 [K]	   
          Upper Temperature = 6000 [K]	   
        END	   
        LOWER INTERVAL COEFFICIENTS:	   
          NASA a1 = 1.25245480E+01 []	   
          NASA a2 = -1.01018826E-02 [K^-1]	   
          NASA a3 = 2.21992610E-04 [K^-2]	   
          NASA a4 = -2.84863722E-07 [K^-3]	   
          NASA a5 = 1.12410138E-10 [K^-4]	   
          NASA a6 = -2.98434398E+04 [K]	   
          NASA a7 = -1.97109989E+01 []	   
        END	   
        UPPER INTERVAL COEFFICIENTS:	   
          NASA a1 = 2.09430708E+01 []	   
          NASA a2 = 4.41691018E-02 [K^-1]	   
          NASA a3 = -1.53261633E-05 [K^-2]	   
          NASA a4 = 2.30544803E-09 [K^-3]	   
          NASA a5 = -1.29765727E-13 [K^-4]	   
          NASA a6 = -3.55755088E+04 [K]	   
          NASA a7 = -8.10637726E+01 []	   
        END	   
      END	   
      REFERENCE STATE:	   
        Option = NASA Format	   
        Reference Pressure = 1 [atm]	   
        Reference Temperature =  298.15 [K]	   
      END      	   
      DYNAMIC VISCOSITY:	   
        Dynamic Viscosity = 0.00050972 [kg/m/s]	   
        Option = Value	   
      END	   
      REFRACTIVE INDEX:	   
        Option = Value	   
        Refractive Index = 1 [m m^-1]	   
      END	   
      SCATTERING COEFFICIENT:	   
        Option = Value	   
        Scattering Coefficient = 0 [m^-1]	   
      END	   
      ABSORPTION COEFFICIENT:	   
        Absorption Coefficient = 1 [m^-1]	   
        Option = Value	   
      END	   
      THERMAL CONDUCTIVITY:	   
        Option = Value	   
        Thermal Conductivity = 0.12445 [W m^-1 K^-1]	   
      END	   
      EQUATION OF STATE:	   
        Molar Mass = 114.231 [kg kmol^-1]	   
        Option = Ideal Gas	   
      END	   
    END	   
  END	   
	   
  MATERIAL:I C8H18	   
    Material Description = Isooctane (2,2,4 trimethylpentane) Vapour (C8H18)	   
    Option = Pure Substance	   
    Thermodynamic State = Gas	   
    Material Group = Gas Phase Combustion	   
    PROPERTIES:	   
      Option = General Material	   
      SPECIFIC HEAT CAPACITY:	   
        Option = NASA Format	   
        TEMPERATURE LIMITS:	   
          Lower Temperature = 200 [K]	   
          Midpoint Temperature = 1000 [K]	   
          Upper Temperature = 6000 [K]	   
        END	   
        LOWER INTERVAL COEFFICIENTS:	   
          NASA a1 = 8.15741071E-01 []	   
          NASA a2 = 7.32647307E-02 [K^-1]	   
          NASA a3 = 1.78301503E-05 [K^-2]	   
          NASA a4 = -6.93592790E-08 [K^-3]	   
          NASA a5 = 3.21630852E-11 [K^-4]	   
          NASA a6 = -3.04774255E+04 [K]	   
          NASA a7 = 2.41511097E+01 []	   
        END	   
        UPPER INTERVAL COEFFICIENTS:	   
          NASA a1 = 1.76160941E+01 []	   
          NASA a2 = 5.13323108E-02 [K^-1]	   
          NASA a3 = -1.65307266E-05 [K^-2]	   
          NASA a4 = 2.43232275E-09 [K^-3]	   
          NASA a5 = -1.35572757E-13 [K^-4]	   
          NASA a6 = -3.63461118E+04 [K]	   
          NASA a7 = -6.86446285E+01 []	   
        END	   
      END	   
      REFERENCE STATE:	   
        Option = NASA Format	   
        Reference Pressure = 1 [atm]	   
        Reference Temperature =  298.15 [K]	   
      END      	   
      DYNAMIC VISCOSITY:	   
        Dynamic Viscosity = 0.000012455 [kg/m/s]	   
        Option = Value	   
      END	   
      REFRACTIVE INDEX:	   
        Option = Value	   
        Refractive Index = 1 [m m^-1]	   
      END	   
      SCATTERING COEFFICIENT:	   
        Option = Value	   
        Scattering Coefficient = 0 [m^-1]	   
      END	   
      ABSORPTION COEFFICIENT:	   
        Absorption Coefficient = 1 [m^-1]	   
        Option = Value	   
      END	   
      THERMAL CONDUCTIVITY:	   
        Option = Value	   
        Thermal Conductivity = 0.028114 [W m^-1 K^-1]	   
      END	   
      EQUATION OF STATE:	   
        Molar Mass = 114.231 [kg kmol^-1]	   
        Option = Ideal Gas	   
      END	   
    END	   
  END	   
	   
  MATERIAL:C9H20	   
    Material Description = N-Nonane Vapour (C9H20)	    
    Option = Pure Substance	   
    Thermodynamic State = Gas	   
    Material Group = Gas Phase Combustion	   
    PROPERTIES:	   
      Option = General Material	   
      SPECIFIC HEAT CAPACITY:	   
        Option = NASA Format	   
        TEMPERATURE LIMITS:	   
          Lower Temperature = 200 [K]	   
          Midpoint Temperature = 1000 [K]	   
          Upper Temperature = 6000 [K]	   
        END	   
        LOWER INTERVAL COEFFICIENTS:	   
          NASA a1 = 1.39840225E+01 []	   
          NASA a2 = -1.17224978E-02 [K^-1]	   
          NASA a3 = 2.52316467E-04 [K^-2]	   
          NASA a4 = -3.25680364E-07 [K^-3]	   
          NASA a5 = 1.29109135E-10 [K^-4]	   
          NASA a6 = -3.28258409E+04 [K]	   
          NASA a7 = -2.38633750E+01 []	   
        END	   
        UPPER INTERVAL COEFFICIENTS:	   
          NASA a1 = 2.55877522E+01 []	   
          NASA a2 = 4.60770651E-02 [K^-1]	   
          NASA a3 = -1.60860633E-05 [K^-2]	   
          NASA a4 = 2.58274408E-09 [K^-3]	   
          NASA a5 = -1.54734690E-13 [K^-4]	   
          NASA a6 = -4.00748448E+04 [K]	   
          NASA a7 = -1.04722466E+02 []	   
        END	   
      END	   
      REFERENCE STATE:	   
        Option = NASA Format	   
        Reference Pressure = 1 [atm]	   
        Reference Temperature =  298.15 [K]	   
      END      	   
      DYNAMIC VISCOSITY:	   
        Dynamic Viscosity = 0.00065402 [kg/m/s]	   
        Option = Value	   
      END	   
      REFRACTIVE INDEX:	   
        Option = Value	   
        Refractive Index = 1 [m m^-1]	   
      END	   
      SCATTERING COEFFICIENT:	   
        Option = Value	   
        Scattering Coefficient = 0 [m^-1]	   
      END	   
      ABSORPTION COEFFICIENT:	   
        Absorption Coefficient = 1 [m^-1]	   
        Option = Value	   
      END	   
      THERMAL CONDUCTIVITY:	   
        Option = Value	   
        Thermal Conductivity = 0.12668 [W m^-1 K^-1]	   
      END	   
      EQUATION OF STATE:	   
        Molar Mass = 128.258 [kg kmol^-1]	   
        Option = Ideal Gas	   
      END	   
    END	   
  END	   
	   
  MATERIAL:C10H22	   
    Material Description = N-Decane Vapour (C10H22)	   
    Option = Pure Substance	   
    Thermodynamic State = Gas	   
    Material Group = Gas Phase Combustion	   
    PROPERTIES:	   
      Option = General Material	   
      SPECIFIC HEAT CAPACITY:	   
        Option = NASA Format	   
        TEMPERATURE LIMITS:	   
          Lower Temperature = 200 [K]	   
          Midpoint Temperature = 1000 [K]	   
          Upper Temperature = 6000 [K]	   
        END	   
        LOWER INTERVAL COEFFICIENTS:	   
          NASA a1 = 1.54328173E+01 []	   
          NASA a2 = -1.32979232E-02 [K^-1]	   
          NASA a3 = 2.82480581E-04 [K^-2]	   
          NASA a4 = -3.65923298E-07 [K^-3]	   
          NASA a5 = 1.45372117E-10 [K^-4]	   
          NASA a6 = -3.58632831E+04 [K]	   
          NASA a7 = -2.79454341E+01 []	   
        END	   
        UPPER INTERVAL COEFFICIENTS:	   
          NASA a1 = 2.94782956E+01 []	   
          NASA a2 = 4.90518943E-02 [K^-1]	   
          NASA a3 = -1.70317179E-05 [K^-2]	   
          NASA a4 = 2.72919300E-09 [K^-3]	   
          NASA a5 = -1.63370772E-13 [K^-4]	   
          NASA a6 = -4.43022624E+04 [K]	   
          NASA a7 = -1.24062121E+02 []	   
        END	   
      END	   
      REFERENCE STATE:	   
        Option = NASA Format	   
        Reference Pressure = 1 [atm]	   
        Reference Temperature =  298.15 [K]	   
      END      	   
      DYNAMIC VISCOSITY:	   
        Dynamic Viscosity = 0.00084812 [kg/m/s]	   
        Option = Value	   
      END	   
      REFRACTIVE INDEX:	   
        Option = Value	   
        Refractive Index = 1 [m m^-1]	   
      END	   
      SCATTERING COEFFICIENT:	   
        Option = Value	   
        Scattering Coefficient = 0 [m^-1]	   
      END	   
      ABSORPTION COEFFICIENT:	   
        Absorption Coefficient = 1 [m^-1]	   
        Option = Value	   
      END	   
      THERMAL CONDUCTIVITY:	   
        Option = Value	   
        Thermal Conductivity = 0.12948 [W m^-1 K^-1]	   
      END	   
      EQUATION OF STATE:	   
        Molar Mass = 142.285 [kg kmol^-1]	   
        Option = Ideal Gas	   
      END	   
    END	   
  END	   
	   
  MATERIAL:C16H34	   
    Material Description = Cetane (Hexadecane) Vapour (C16H34)	   
    Option = Pure Substance	   
    Thermodynamic State = Gas	   
    Material Group = Gas Phase Combustion	   
    PROPERTIES:	   
      Option = General Material	   
      SPECIFIC HEAT CAPACITY:	   
        Option = NASA Format	   
        TEMPERATURE LIMITS:	   
          Lower Temperature = 298.15 [K]	   
          Midpoint Temperature = 1000 [K]	   
          Upper Temperature = 5000 [K]	   
        END	   
        LOWER INTERVAL COEFFICIENTS:	   
          NASA a1 = -2.28147400E+00 []	   
          NASA a2 = 1.85127971E-01 [K^-1]	   
          NASA a3 = -9.91782207E-05 [K^-2]	   
          NASA a4 = 1.43398377E-08 [K^-3]	   
          NASA a5 = 3.73230542E-12 [K^-4]	   
          NASA a6 = -5.17449265E+04 [K]	   
          NASA a7 = 5.60024917E+01 []	   
        END	   
        UPPER INTERVAL COEFFICIENTS:	   
          NASA a1 = 3.93197519E+01 []	   
          NASA a2 = 9.11470601E-02 [K^-1]	   
          NASA a3 = -3.39721140E-05 [K^-2]	   
          NASA a4 = 5.94437262E-09 [K^-3]	   
          NASA a5 = -3.95796331E-13 [K^-4]	   
          NASA a6 = -6.51665791E+04 [K]	   
          NASA a7 = -1.66160224E+02 []	   
        END	   
      END	   
      REFERENCE STATE:	   
        Option = NASA Format	   
        Reference Pressure = 1 [atm]	   
        Reference Temperature =  298.15 [K]	   
      END      	   
      DYNAMIC VISCOSITY:	   
        Dynamic Viscosity = 0.000010363 [kg/m/s]	   
        Option = Value	   
      END	   
      REFRACTIVE INDEX:	   
        Option = Value	   
        Refractive Index = 1 [m m^-1]	   
      END	   
      SCATTERING COEFFICIENT:	   
        Option = Value	   
        Scattering Coefficient = 0 [m^-1]	   
      END	   
      ABSORPTION COEFFICIENT:	   
        Absorption Coefficient = 1 [m^-1]	   
        Option = Value	   
      END	   
      THERMAL CONDUCTIVITY:	   
        Option = Value	   
        Thermal Conductivity = 0.0028214 [W m^-1 K^-1]	   
      END	   
      EQUATION OF STATE:	   
        Molar Mass = 226.446 [kg kmol^-1]	   
        Option = Ideal Gas	   
      END	   
    END	   
  END

  MATERIAL: JetA
    Material Description = Vapour Jet-A Fuel (C12H23)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      EQUATION OF STATE:
        Option = Ideal Gas
        Molar Mass = 167.31462 [kg kmol^-1]
      END
      DYNAMIC VISCOSITY:
        Option = Value
        Dynamic Viscosity = 5.E-06 [kg m^-1 s^-1]
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 1.E-02 [W m^-1 K^-1]
      END
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 273.15 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 =  2.08692170E+00 []
          NASA a2 =  1.33149650E-01 [K^-1]
          NASA a3 = -8.11574520E-05 [K^-2]
          NASA a4 =  2.94092860E-08 [K^-3]
          NASA a5 = -6.51952130E-12 [K^-4]
          NASA a6 = -3.59128140E+04 [K]
          NASA a7 =  2.73552890E+01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 =  2.48802010E+01 []
          NASA a2 =  7.82500480E-02 [K^-1]
          NASA a3 = -3.15509730E-05 [K^-2]
          NASA a4 =  5.78789000E-09 [K^-3]
          NASA a5 = -3.98279680E-13 [K^-4]
          NASA a6 = -4.31106840E+04 [K]
          NASA a7 = -9.36552550E+01 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END
      ABSORPTION COEFFICIENT:
        Option = Value
        Absorption Coefficient = 1.0 [m^-1]
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
    END
  END

  MATERIAL:CO
    Material Description = Carbon Monoxide CO 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.03262452E+02 []
          NASA a2 = 0.01511941E-01 [K^-1]
          NASA a3 = -0.03881755E-04 [K^-2]
          NASA a4 = 0.05581944E-07 [K^-3]
          NASA a5 = -0.02474951E-10 [K^-4]
          NASA a6 = -0.01431054E+06 [K]
          NASA a7 = 0.04848897E+02 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.03025078E+02 []
          NASA a2 = 0.01442689E-01 [K^-1]
          NASA a3 = -0.05630828E-05 [K^-2]
          NASA a4 = 0.01018581E-08 [K^-3]
          NASA a5 = -0.06910952E-13 [K^-4]
          NASA a6 = -0.01426835E+06 [K]
          NASA a7 = 0.06108218E+02 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 16.6E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 251E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 28.01 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:CO2
    Material Description = Carbon Dioxide CO2 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.02275725E+02 []
          NASA a2 = 0.09922072E-01 [K^-1]
          NASA a3 = -0.01040911E-03 [K^-2]
          NASA a4 = 0.06866687E-07 [K^-3]
          NASA a5 = -0.02117280E-10 [K^-4]
          NASA a6 = -0.04837314E+06 [K]
          NASA a7 = 0.01018849E+03 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.04453623E+02 []
          NASA a2 = 0.03140169E-01 [K^-1]
          NASA a3 = -0.01278411E-04 [K^-2]
          NASA a4 = 0.02393997E-08 [K^-3]
          NASA a5 = -0.01669033E-12 [K^-4]
          NASA a6 = -0.04896696E+06 [K]
          NASA a7 = -0.09553959E+01 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 14.9E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 145E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 44.01 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:H
    Material Description = Atomic Hydrogen H 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.02500000E+02 []
          NASA a2 = 0.00000000E+00 [K^-1]
          NASA a3 = 0.00000000E+00 [K^-2]
          NASA a4 = 0.00000000E+00 [K^-3]
          NASA a5 = 0.00000000E+00 [K^-4]
          NASA a6 = 0.02547163E+06 [K]
          NASA a7 = -0.04601176E+01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.02500000E+02 []
          NASA a2 = 0.00000000E+00 [K^-1]
          NASA a3 = 0.00000000E+00 [K^-2]
          NASA a4 = 0.00000000E+00 [K^-3]
          NASA a5 = 0.00000000E+00 [K^-4]
          NASA a6 = 0.02547163E+06 [K]
          NASA a7 = -0.04601176E+01 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 1.81E-5 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 3.E-2 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 1.01 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:H2
    Material Description = Hydrogen H2 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.03298124E+02 []
          NASA a2 = 0.08249442E-02 [K^-1]
          NASA a3 = -0.08143015E-05 [K^-2]
          NASA a4 = -0.09475434E-09 [K^-3]
          NASA a5 = 0.04134872E-11 [K^-4]
          NASA a6 = -0.01012521E+05 [K]
          NASA a7 = -0.03294094E+02 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.02991423E+02 []
          NASA a2 = 0.07000644E-02 [K^-1]
          NASA a3 = -0.05633829E-06 [K^-2]
          NASA a4 = -0.09231578E-10 [K^-3]
          NASA a5 = 0.01582752E-13 [K^-4]
          NASA a6 = -0.08350340E+04 [K]
          NASA a7 = -0.01355110E+02 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 8.8E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 1.809E-01 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 2.016 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:H2NO
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1500 [K]
          Upper Temperature = 4000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 2.5305890E+00 []
          NASA a2 = 8.5960350E-03 [K^-1]
          NASA a3 = -5.4710300E-06 [K^-2]
          NASA a4 = 2.2762490E-09 [K^-3]
          NASA a5 = -4.6480730E-13 [K^-4]
          NASA a6 = 6.8680300E+03 [K]
          NASA a7 = 1.1266506E+01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 5.6733460E+00 []
          NASA a2 = 2.2988360E-03 [K^-1]
          NASA a3 = -1.7744450E-07 [K^-2]
          NASA a4 = -1.1034818E-10 [K^-3]
          NASA a5 = 1.8597620E-14 [K^-4]
          NASA a6 = 5.5693250E+03 [K]
          NASA a7 = -6.1535400E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 32.02 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:H2O
    Material Description = Water Vapour 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion, Interphase Mass Transfer, Water Data
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.03386842E+02 []
          NASA a2 = 0.03474982E-01 [K^-1]
          NASA a3 = -0.06354696E-04 [K^-2]
          NASA a4 = 0.06968581E-07 [K^-3]
          NASA a5 = -0.02506588E-10 [K^-4]
          NASA a6 = -0.03020811E+06 [K]
          NASA a7 = 0.02590233E+02 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.02672146E+02 []
          NASA a2 = 0.03056293E-01 [K^-1]
          NASA a3 = -0.08730260E-05 [K^-2]
          NASA a4 = 0.01200996E-08 [K^-3]
          NASA a5 = -0.06391618E-13 [K^-4]
          NASA a6 = -0.02989921E+06 [K]
          NASA a7 = 0.06862817E+02 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 9.4E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 193E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 18.02 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:H2O2
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 3.3887530E+00 []
          NASA a2 = 6.5692260E-03 [K^-1]
          NASA a3 = -1.4850125E-07 [K^-2]
          NASA a4 = -4.6258050E-09 [K^-3]
          NASA a5 = 2.4715140E-12 [K^-4]
          NASA a6 = -1.7663140E+04 [K]
          NASA a7 = 6.7853630E+00 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 4.5731670E+00 []
          NASA a2 = 4.3361360E-03 [K^-1]
          NASA a3 = -1.4746888E-06 [K^-2]
          NASA a4 = 2.3489030E-10 [K^-3]
          NASA a5 = -1.4316536E-14 [K^-4]
          NASA a6 = -1.8006960E+04 [K]
          NASA a7 = 5.0113690E-01 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 34.01 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:H2S
    Material Description = Hydrogen Sulphide H2S 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.03071029E+02 []
          NASA a2 = 0.05578261E-01 [K^-1]
          NASA a3 = -0.10309669E-04 [K^-2]
          NASA a4 = 0.12019529E-07 [K^-3]
          NASA a5 = -0.04838369E-10 [K^-4]
          NASA a6 = -0.03559826E+05 [K]
          NASA a7 = 0.05935226E+02 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.02883147E+02 []
          NASA a2 = 0.03827835E-01 [K^-1]
          NASA a3 = -0.14233978E-05 [K^-2]
          NASA a4 = 0.02497998E-08 [K^-3]
          NASA a5 = -0.16602733E-13 [K^-4]
          NASA a6 = -0.03480742E+05 [K]
          NASA a7 = 0.07258161E+02 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 12.9E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 145E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 34.08 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:HCCO
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 4000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 5.0479650E+00 []
          NASA a2 = 4.4534780E-03 [K^-1]
          NASA a3 = 2.2682820E-07 [K^-2]
          NASA a4 = -1.4820945E-09 [K^-3]
          NASA a5 = 2.2507410E-13 [K^-4]
          NASA a6 = 1.9658910E+04 [K]
          NASA a7 = 4.8184390E-01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 6.7580730E+00 []
          NASA a2 = 2.0004000E-03 [K^-1]
          NASA a3 = -2.0276070E-07 [K^-2]
          NASA a4 = -1.0411318E-10 [K^-3]
          NASA a5 = 1.9651640E-14 [K^-4]
          NASA a6 = 1.9015130E+04 [K]
          NASA a7 = -9.0712620E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 41.03 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:HCN
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 2.4904620E+00 []
          NASA a2 = 8.6112800E-03 [K^-1]
          NASA a3 = -1.0310342E-05 [K^-2]
          NASA a4 = 7.4814980E-09 [K^-3]
          NASA a5 = -2.2291090E-12 [K^-4]
          NASA a6 = 1.5208344E+04 [K]
          NASA a7 = 7.9049810E+00 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 3.6500770E+00 []
          NASA a2 = 3.4609980E-03 [K^-1]
          NASA a3 = -1.2742788E-06 [K^-2]
          NASA a4 = 2.2176550E-10 [K^-3]
          NASA a5 = -1.4771774E-14 [K^-4]
          NASA a6 = 1.4983916E+04 [K]
          NASA a7 = 2.3932200E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 27.03 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:HCO
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 2.8983290E+00 []
          NASA a2 = 6.1991460E-03 [K^-1]
          NASA a3 = -9.6230840E-06 [K^-2]
          NASA a4 = 1.0898249E-08 [K^-3]
          NASA a5 = -4.5748850E-12 [K^-4]
          NASA a6 = 4.1599220E+03 [K]
          NASA a7 = 8.9836140E+00 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 3.5572710E+00 []
          NASA a2 = 3.3455720E-03 [K^-1]
          NASA a3 = -1.3350060E-06 [K^-2]
          NASA a4 = 2.4705720E-10 [K^-3]
          NASA a5 = -1.7138500E-14 [K^-4]
          NASA a6 = 3.9163240E+03 [K]
          NASA a7 = 5.5522990E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 29.02 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:HNCO
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 4000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 3.6940590E+00 []
          NASA a2 = 6.6572360E-03 [K^-1]
          NASA a3 = -5.0544680E-08 [K^-2]
          NASA a4 = -3.4734110E-09 [K^-3]
          NASA a5 = 1.3605694E-12 [K^-4]
          NASA a6 = -1.3919758E+04 [K]
          NASA a7 = 5.7127420E+00 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 6.2118670E+00 []
          NASA a2 = 2.2971370E-03 [K^-1]
          NASA a3 = -2.2161280E-07 [K^-2]
          NASA a4 = -1.2220438E-10 [K^-3]
          NASA a5 = 2.2724060E-14 [K^-4]
          NASA a6 = -1.4770725E+04 [K]
          NASA a7 = -8.0166330E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 43.03 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:HNO
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 2.7844020E+00 []
          NASA a2 = 6.6096460E-03 [K^-1]
          NASA a3 = -9.3002230E-06 [K^-2]
          NASA a4 = 9.4379800E-09 [K^-3]
          NASA a5 = -3.7531460E-12 [K^-4]
          NASA a6 = 1.0918779E+04 [K]
          NASA a7 = 9.0356290E+00 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 3.6151440E+00 []
          NASA a2 = 3.2124850E-03 [K^-1]
          NASA a3 = -1.2603370E-06 [K^-2]
          NASA a4 = 2.2672970E-10 [K^-3]
          NASA a5 = -1.5362358E-14 [K^-4]
          NASA a6 = 1.0661911E+04 [K]
          NASA a7 = 4.8102630E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 31.01 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:HO2
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.02979963E+02 []
          NASA a2 = 0.04996697E-01 [K^-1]
          NASA a3 = -0.03790997E-04 [K^-2]
          NASA a4 = 0.02354192E-07 [K^-3]
          NASA a5 = -0.08089024E-11 [K^-4]
          NASA a6 = 0.01762274E+04 [K]
          NASA a7 = 0.09222724E+02 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.04072191E+02 []
          NASA a2 = 0.02131296E-01 [K^-1]
          NASA a3 = -0.05308145E-05 [K^-2]
          NASA a4 = 0.06112269E-09 [K^-3]
          NASA a5 = -0.02841165E-13 [K^-4]
          NASA a6 = -0.01579727E+04 [K]
          NASA a7 = 0.03476029E+02 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 1.81E-5 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 3.E-2 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 33.01 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:HONO
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 2.2904130E+00 []
          NASA a2 = 1.4099223E-02 [K^-1]
          NASA a3 = -1.3678717E-05 [K^-2]
          NASA a4 = 7.4987800E-09 [K^-3]
          NASA a5 = -1.8769050E-12 [K^-4]
          NASA a6 = -1.0431945E+04 [K]
          NASA a7 = 1.3280769E+01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 5.4868920E+00 []
          NASA a2 = 4.2180640E-03 [K^-1]
          NASA a3 = -1.6491426E-06 [K^-2]
          NASA a4 = 2.9718760E-10 [K^-3]
          NASA a5 = -2.0211480E-14 [K^-4]
          NASA a6 = -1.1268646E+04 [K]
          NASA a7 = -2.9970020E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 47.01 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:He
    Material Description = Helium He 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.02500000E+02 []
          NASA a2 = 0.00000000E+00 [K^-1]
          NASA a3 = 0.00000000E+00 [K^-2]
          NASA a4 = 0.00000000E+00 [K^-3]
          NASA a5 = 0.00000000E+00 [K^-4]
          NASA a6 = -0.07453750E+04 [K]
          NASA a7 = 0.09153488E+01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.02500000E+02 []
          NASA a2 = 0.00000000E+00 [K^-1]
          NASA a3 = 0.00000000E+00 [K^-2]
          NASA a4 = 0.00000000E+00 [K^-3]
          NASA a5 = 0.00000000E+00 [K^-4]
          NASA a6 = -0.07453750E+04 [K]
          NASA a7 = 0.09153489E+01 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 18.6E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 1415E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 4.00 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:N
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 2.5030710E+00 []
          NASA a2 = -2.1800180E-05 [K^-1]
          NASA a3 = 5.4205290E-08 [K^-2]
          NASA a4 = -5.6475600E-11 [K^-3]
          NASA a5 = 2.0999040E-14 [K^-4]
          NASA a6 = 5.6098900E+04 [K]
          NASA a7 = 4.1675660E+00 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 2.4502680E+00 []
          NASA a2 = 1.0661458E-04 [K^-1]
          NASA a3 = -7.4653370E-08 [K^-2]
          NASA a4 = 1.8796520E-11 [K^-3]
          NASA a5 = -1.0259839E-15 [K^-4]
          NASA a6 = 5.6116040E+04 [K]
          NASA a7 = 4.4487580E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 14.01 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:N2
    Material Description = Nitrogen N2 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.03298677E+02 []
          NASA a2 = 0.01408240E-01 [K^-1]
          NASA a3 = -0.03963222E-04 [K^-2]
          NASA a4 = 0.05641515E-07 [K^-3]
          NASA a5 = -0.02444855E-10 [K^-4]
          NASA a6 = -0.01020900E+05 [K]
          NASA a7 = 0.03950372E+02 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.02926640E+02 []
          NASA a2 = 0.01487977E-01 [K^-1]
          NASA a3 = -0.05684761E-05 [K^-2]
          NASA a4 = 0.01009704E-08 [K^-3]
          NASA a5 = -0.06753351E-13 [K^-4]
          NASA a6 = -0.09227977E+04 [K]
          NASA a7 = 0.05980528E+02 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 28.01 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:N2O
    Material Description = Nitrous Oxide N2O 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 2.5430570E+00 []
          NASA a2 = 9.4921930E-03 [K^-1]
          NASA a3 = -9.7927750E-06 [K^-2]
          NASA a4 = 6.2638440E-09 [K^-3]
          NASA a5 = -1.9018250E-12 [K^-4]
          NASA a6 = 8.7651000E+03 [K]
          NASA a7 = 9.5112220E+00 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 4.7189770E+00 []
          NASA a2 = 2.8737130E-03 [K^-1]
          NASA a3 = -1.1974958E-06 [K^-2]
          NASA a4 = 2.2505510E-10 [K^-3]
          NASA a5 = -1.5753370E-14 [K^-4]
          NASA a6 = 8.1658110E+03 [K]
          NASA a7 = -1.6572504E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 13.5E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 151E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 44.01 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:NO
    Material Description = Nitric Oxide NO 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.03376542E+02 []
          NASA a2 = 0.01253063E-01 [K^-1]
          NASA a3 = -0.03302751E-04 [K^-2]
          NASA a4 = 0.05217810E-07 [K^-3]
          NASA a5 = -0.02446263E-10 [K^-4]
          NASA a6 = 0.09817961E+05 [K]
          NASA a7 = 0.05829590E+02 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.03245435E+02 []
          NASA a2 = 0.01269138E-01 [K^-1]
          NASA a3 = -0.05015890E-05 [K^-2]
          NASA a4 = 0.09169283E-09 [K^-3]
          NASA a5 = -0.06275419E-13 [K^-4]
          NASA a6 = 0.09800840E+05 [K]
          NASA a7 = 0.06417294E+02 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.8E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 238E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 30.01 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:NCO
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 2.8303200E+00 []
          NASA a2 = 8.8714900E-03 [K^-1]
          NASA a3 = -8.9456360E-06 [K^-2]
          NASA a4 = 5.8769180E-09 [K^-3]
          NASA a5 = -1.9077340E-12 [K^-4]
          NASA a6 = 1.8005430E+04 [K]
          NASA a7 = 9.4988310E+00 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 5.0120450E+00 []
          NASA a2 = 2.6267730E-03 [K^-1]
          NASA a3 = -1.1082433E-06 [K^-2]
          NASA a4 = 2.0938600E-10 [K^-3]
          NASA a5 = -1.4603470E-14 [K^-4]
          NASA a6 = 1.7371850E+04 [K]
          NASA a7 = -1.8300750E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 42.02 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:NH
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 3.3397580E+00 []
          NASA a2 = 1.2530086E-03 [K^-1]
          NASA a3 = -3.4916450E-06 [K^-2]
          NASA a4 = 4.2188120E-09 [K^-3]
          NASA a5 = -1.5576179E-12 [K^-4]
          NASA a6 = 4.1850470E+04 [K]
          NASA a7 = 2.5071800E+00 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 2.7602490E+00 []
          NASA a2 = 1.3753463E-03 [K^-1]
          NASA a3 = -4.4519140E-07 [K^-2]
          NASA a4 = 7.6927910E-11 [K^-3]
          NASA a5 = -5.0175920E-15 [K^-4]
          NASA a6 = 4.2078280E+04 [K]
          NASA a7 = 5.8571990E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 15.01 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:NH2
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 3.4324930E+00 []
          NASA a2 = 3.2995400E-03 [K^-1]
          NASA a3 = -6.6136000E-06 [K^-2]
          NASA a4 = 8.5909470E-09 [K^-3]
          NASA a5 = -3.5720460E-12 [K^-4]
          NASA a6 = 2.1772270E+04 [K]
          NASA a7 = 3.0901100E+00 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 2.9613110E+00 []
          NASA a2 = 2.9326990E-03 [K^-1]
          NASA a3 = -9.0636000E-07 [K^-2]
          NASA a4 = 1.6172575E-10 [K^-3]
          NASA a5 = -1.2042003E-14 [K^-4]
          NASA a6 = 2.1919760E+04 [K]
          NASA a7 = 5.7778780E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 16.02 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:NH3
    Material Description = Ammonia NH3 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 2.2043510E+00 []
          NASA a2 = 1.0114765E-02 [K^-1]
          NASA a3 = -1.4652648E-05 [K^-2]
          NASA a4 = 1.4472350E-08 [K^-3]
          NASA a5 = -5.3285090E-12 [K^-4]
          NASA a6 = -6.5254880E+03 [K]
          NASA a7 = 8.1271380E+00 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 2.4619040E+00 []
          NASA a2 = 6.0591660E-03 [K^-1]
          NASA a3 = -2.0049760E-06 [K^-2]
          NASA a4 = 3.1360030E-10 [K^-3]
          NASA a5 = -1.9383170E-14 [K^-4]
          NASA a6 = -6.4932690E+03 [K]
          NASA a7 = 7.4720970E+00 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 10.3E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 245E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 17.03 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:NO2
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 2.6706000E+00 []
          NASA a2 = 7.8385000E-03 [K^-1]
          NASA a3 = -8.0638640E-06 [K^-2]
          NASA a4 = 6.1617140E-09 [K^-3]
          NASA a5 = -2.3201500E-12 [K^-4]
          NASA a6 = 2.8962900E+03 [K]
          NASA a7 = 1.1612071E+01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 4.6828590E+00 []
          NASA a2 = 2.4624290E-03 [K^-1]
          NASA a3 = -1.0422585E-06 [K^-2]
          NASA a4 = 1.9769020E-10 [K^-3]
          NASA a5 = -1.3917168E-14 [K^-4]
          NASA a6 = 2.2612920E+03 [K]
          NASA a7 = 9.8859850E-01 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 46.01 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:O
    Material Description = Atomic Oxygen O 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.02946429E+02 []
          NASA a2 = -0.01638166E-01 [K^-1]
          NASA a3 = 0.02421032E-04 [K^-2]
          NASA a4 = -0.01602843E-07 [K^-3]
          NASA a5 = 0.03890696E-11 [K^-4]
          NASA a6 = 0.02914764E+06 [K]
          NASA a7 = 0.02963995E+02 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.02542060E+02 []
          NASA a2 = -0.02755062E-03 [K^-1]
          NASA a3 = -0.03102803E-07 [K^-2]
          NASA a4 = 0.04551067E-10 [K^-3]
          NASA a5 = -0.04368052E-14 [K^-4]
          NASA a6 = 0.02923080E+06 [K]
          NASA a7 = 0.04920308E+02 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 470E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 16.00 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:O2
    Material Description = Oxygen O2 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.03212936E+02 []
          NASA a2 = 0.01127486E-01 [K^-1]
          NASA a3 = -0.05756150E-05 [K^-2]
          NASA a4 = 0.01313877E-07 [K^-3]
          NASA a5 = -0.08768554E-11 [K^-4]
          NASA a6 = -0.01005249E+05 [K]
          NASA a7 = 0.06034738E+02 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.03697578E+02 []
          NASA a2 = 0.06135197E-02 [K^-1]
          NASA a3 = -0.01258842E-05 [K^-2]
          NASA a4 = 0.01775281E-09 [K^-3]
          NASA a5 = -0.01136435E-13 [K^-4]
          NASA a6 = -0.01233930E+05 [K]
          NASA a7 = 0.03189166E+02 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 19.2E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 266E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 31.99 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:OH
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.03637266E+02 []
          NASA a2 = 0.01850910E-02 [K^-1]
          NASA a3 = -0.01676165E-04 [K^-2]
          NASA a4 = 0.02387203E-07 [K^-3]
          NASA a5 = -0.08431442E-11 [K^-4]
          NASA a6 = 0.03606782E+05 [K]
          NASA a7 = 0.01358860E+02 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.02882730E+02 []
          NASA a2 = 0.01013974E-01 [K^-1]
          NASA a3 = -0.02276877E-05 [K^-2]
          NASA a4 = 0.02174684E-09 [K^-3]
          NASA a5 = -0.05126305E-14 [K^-4]
          NASA a6 = 0.03886888E+05 [K]
          NASA a7 = 0.05595712E+02 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 1.81E-5 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 3.E-2 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 17.01 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

  MATERIAL:SO2
    Material Description = Sulphur Dioxide SO2 
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Gas Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 300 [K]
          Midpoint Temperature = 1000 [K]
          Upper Temperature = 5000 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 = 0.02911438E+02 []
          NASA a2 = 0.08103022E-01 [K^-1]
          NASA a3 = -0.06906710E-04 [K^-2]
          NASA a4 = 0.03329015E-07 [K^-3]
          NASA a5 = -0.08777121E-11 [K^-4]
          NASA a6 = -0.03687881E+06 [K]
          NASA a7 = 0.11117403E+02 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 = 0.05254498E+02 []
          NASA a2 = 0.01978545E-01 [K^-1]
          NASA a3 = -0.08204226E-05 [K^-2]
          NASA a4 = 0.15763830E-09 [K^-3]
          NASA a5 = -0.11204512E-13 [K^-4]
          NASA a6 = -0.03756885E+06 [K]
          NASA a7 = -0.11460563E+01 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 16.5E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 77E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 64.06 [kg kmol^-1]
        Option = Ideal Gas
      END
    END
  END

########################################################################
# Gases with constant properties at STP (0 C and 1 atm)
########################################################################

  MATERIAL:CH4 at STP
    Material Description = Methane CH4 at STP (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Constant Property Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 11.1E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 343E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 0.717 [kg m^-3]
        Molar Mass = 16.04 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2210 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = -4.7232670E+06 [J/kg]
        Reference Specific Entropy = 1.1405054E+04 [J/kg/K]
        Reference Temperature = 0 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 0.00366 [K^-1]
      END
    END
  END

  MATERIAL:CO at STP
    Material Description = Carbon Monoxide CO at STP (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Constant Property Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 16.6E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 251E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 1.250 [kg m^-3]
        Molar Mass = 28.01 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1040 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = -3.9723161E+06 [J/kg]
        Reference Specific Entropy = 6.9616565E+03 [J/kg/K]
        Reference Temperature = 0 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 0.00366 [K^-1]
      END
    END
  END

  MATERIAL:CO2 at STP
    Material Description = Carbon Dioxide CO2 at STP (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Constant Property Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 14.9E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 145E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 1.977 [kg m^-3]
        Molar Mass = 44.01 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 851 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = -8.9632991E+06 [J/kg]
        Reference Specific Entropy = 4.7823107E+03 [J/kg/K]
        Reference Temperature = 0 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 0.00366 [K^-1]
      END
    END
  END

  MATERIAL:H2 at STP
    Material Description = Hydrogen H2 at STP (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Constant Property Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 8.8E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 1.809E-01 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 0.09 [kg m^-3]
        Molar Mass = 2.016 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 14300 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = -3.5690060E+05 [J/kg]
        Reference Specific Entropy = 6.3527621E+04 [J/kg/K]
        Reference Temperature = 0 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 0.00366 [K^-1]
      END
    END
  END

  MATERIAL:H2S at STP
    Material Description = Hydrogen Sulphide H2S at STP (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Constant Property Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 12.9E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 145E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 1.538 [kg m^-3]
        Molar Mass = 34.08 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1000 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = -6.2657098E+05 [J/kg]
        Reference Specific Entropy = 5.9463044E+03 [J/kg/K]
        Reference Temperature = 0 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 0.00366 [K^-1]
      END
    END
  END

  MATERIAL:He at STP
    Material Description = Helium He at STP (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Constant Property Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 18.6E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 1415E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 0.179 [kg m^-3]
        Molar Mass = 4.00 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 5240 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = -1.2982658E+05 [J/kg]
        Reference Specific Entropy = 3.1034571E+04 [J/kg/K]
        Reference Temperature = 0 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 0.00366 [K^-1]
      END
    END
  END

  MATERIAL:N2 at STP
    Material Description = Nitrogen N2 at STP (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Constant Property Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 1.250 [kg m^-3]
        Molar Mass = 28.01 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1040 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = -2.5896365E+04 [J/kg]
        Reference Specific Entropy = 6.7454037E+03 [J/kg/K]
        Reference Temperature = 0 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 0.00366 [K^-1]
      END
    END
  END

  MATERIAL:N2O at STP
    Material Description = Nitrous Oxide N2O at STP (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Constant Property Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 13.5E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 151E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 1.978 [kg m^-3]
        Molar Mass = 44.01 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 892 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = 1.8425118E+06 [J/kg]
        Reference Specific Entropy = 4.9188411E+03 [J/kg/K]
        Reference Temperature = 0 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 0.00366 [K^-1]
      END
    END
  END

  MATERIAL:NH3 at STP
    Material Description = Ammonia NH3 at STP (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Constant Property Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 10.3E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 245E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 0.771 [kg m^-3]
        Molar Mass = 17.03 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2090 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = -2.7479549E+06 [J/kg]
        Reference Specific Entropy = 1.1128326E+04 [J/kg/K]
        Reference Temperature = 0 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 0.00366 [K^-1]
      END
    END
  END

  MATERIAL:NO at STP
    Material Description = Nitric Oxide NO at STP (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Constant Property Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.8E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 238E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 1.340 [kg m^-3]
        Molar Mass = 30.01 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 972 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = 2.9844835E+06 [J/kg]
        Reference Specific Entropy = 6.9334362E+03 [J/kg/K]
        Reference Temperature = 0 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 0.00366 [K^-1]
      END
    END
  END

  MATERIAL:O2 at STP
    Material Description = Oxygen O2 at STP (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Constant Property Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 19.2E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 266E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 1.429 [kg m^-3]
        Molar Mass = 32.00 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 920 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = -2.2942475E+04 [J/kg]
        Reference Specific Entropy = 6.3274847E+03 [J/kg/K]
        Reference Temperature = 0 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 0.00366 [K^-1]
      END
    END
  END

  MATERIAL:SO2 at STP
    Material Description = Sulphur Dioxide SO2 at STP (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Constant Property Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 16.5E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 77E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 2.927 [kg m^-3]
        Molar Mass = 64.06 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 625 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = -4.6494247E+06 [J/kg]
        Reference Specific Entropy = 3.8183106E+03 [J/kg/K]
        Reference Temperature = 0 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 0.00366 [K^-1]
      END
    END
  END

########################################################################
# Ideal Gases with constant Cp at STP (0 C and 1 atm)
########################################################################

  MATERIAL:CH4 Ideal Gas
    Material Description = Methane CH4 Ideal Gas (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Calorically Perfect Ideal Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 11.1E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 343E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 16.04 [kg kmol^-1]
        Option = Ideal Gas
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2210 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature = 0 [C]
      END
    END
  END

  MATERIAL:CO Ideal Gas
    Material Description = Carbon Monoxide CO Ideal Gas (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Calorically Perfect Ideal Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 16.6E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 251E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 28.01 [kg kmol^-1]
        Option = Ideal Gas
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1040 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature = 0 [C]
      END
    END
  END

  MATERIAL:CO2 Ideal Gas
    Material Description = Carbon Dioxide CO2 Ideal Gas (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Calorically Perfect Ideal Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 14.9E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 145E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 44.01 [kg kmol^-1]
        Option = Ideal Gas
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 851 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature = 0 [C]
      END
    END
  END

  MATERIAL:H2 Ideal Gas
    Material Description = Hydrogen H2 Ideal Gas (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Calorically Perfect Ideal Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 8.8E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 1.809E-01 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 2.016 [kg kmol^-1]
        Option = Ideal Gas
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 14300 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature = 0 [C]
      END
    END
  END

  MATERIAL:H2S Ideal Gas
    Material Description = Hydrogen Sulphide H2S Ideal Gas (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Calorically Perfect Ideal Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 12.9E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 145E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 34.08 [kg kmol^-1]
        Option = Ideal Gas
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1000 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature = 0 [C]
      END
    END
  END

  MATERIAL:He Ideal Gas
    Material Description = Helium He Ideal Gas (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Calorically Perfect Ideal Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 18.6E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 1415E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 4.00 [kg kmol^-1]
        Option = Ideal Gas
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 5240 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature = 0 [C]
      END
    END
  END

  MATERIAL:N2 Ideal Gas
    Material Description = Nitrogen N2 Ideal Gas (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Calorically Perfect Ideal Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.7E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 259E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 28.01 [kg kmol^-1]
        Option = Ideal Gas
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1040 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature = 0 [C]
      END
    END
  END

  MATERIAL:N2O Ideal Gas
    Material Description = Nitrous Oxide N2O Ideal Gas (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Calorically Perfect Ideal Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 13.5E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 151E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 44.01 [kg kmol^-1]
        Option = Ideal Gas
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 892 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature = 0 [C]
      END
    END
  END

  MATERIAL:NO2 Ideal Gas
    Material Description = Nitrous Dioxide NO2 Ideal Gas (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Calorically Perfect Ideal Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 13.2E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 14.57E-03 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 46.01 [kg kmol^-1]
        Option = Ideal Gas
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 789 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature = 0 [C]
      END
    END
  END

  MATERIAL:NH3 Ideal Gas
    Material Description = Ammonia NH3 Ideal Gas (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Calorically Perfect Ideal Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 10.3E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 245E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 17.03 [kg kmol^-1]
        Option = Ideal Gas
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2090 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature = 0 [C]
      END
    END
  END

  MATERIAL:NO Ideal Gas
    Material Description = Nitric Oxide NO Ideal Gas (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Calorically Perfect Ideal Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 17.8E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 238E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 30.01 [kg kmol^-1]
        Option = Ideal Gas
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 972 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature = 0 [C]
      END
    END
  END

  MATERIAL:O2 Ideal Gas
    Material Description = Oxygen O2 Ideal Gas (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Calorically Perfect Ideal Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 19.2E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 266E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 32.00 [kg kmol^-1]
        Option = Ideal Gas
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 920 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature = 0 [C]
      END
    END
  END

  MATERIAL:SO2 Ideal Gas
    Material Description = Sulphur Dioxide SO2 Ideal Gas (0 C and 1 atm)
    Option = Pure Substance
    Thermodynamic State = Gas
    Material Group = Calorically Perfect Ideal Gases
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 16.5E-06 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 77E-04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 64.06 [kg kmol^-1]
        Option = Ideal Gas
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 625 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature = 0 [C]
      END
    END
  END

########################################################################
# Liquids
########################################################################

# References:
# ***********
# [Ref 1] Science Data Book, R.M. Tennent
# [Ref 2] Fundamentals of Heat and Mass Transfer, 2nd Ed.,
#         F.P.Incropera & D.P. De Witt
# [Ref 3] CRC Handbook of Chemistry and Physics
# [Ref 4] Perry's Chemical Engineers' Handbook 6th Edition.

  MATERIAL:Acetone C3H6O
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Constant Property Liquids
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.324E-03 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.161 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 780 [kg m^-3]
        Molar Mass = 58.08 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2210 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 14.3E-04 [K^-1]
      END
    END
  END

  MATERIAL:Ethanol C2H6O
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Constant Property Liquids
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 1.197E-03 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.177 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 789 [kg m^-3]
        Molar Mass = 46.07 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2500 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 10.8E-04 [K^-1]
      END
    END
  END

  MATERIAL:Glycerol C3H8O3
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Constant Property Liquids
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 1495E-03 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.27 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 1262 [kg m^-3]
        Molar Mass = 92.09 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2400 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 4.7E-04 [K^-1]
      END
    END
  END

  MATERIAL:Mercury Hg
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Constant Property Liquids
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 1.552E-03 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 7.96 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 13546 [kg m^-3]
        Molar Mass = 200.59 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 140 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 1.82E-04 [K^-1]
      END
    END
  END

  MATERIAL:Methanol CH4O
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Constant Property Liquids
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.594E-03 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.201 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 791 [kg m^-3]
        Molar Mass = 32.04 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2500 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 11.9E-04 [K^-1]
      END
    END
  END

  MATERIAL:Nitrobenzene C6H5NO2
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Constant Property Liquids
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 2.03E-03 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.16 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 1175 [kg m^-3]
        Molar Mass = 123.11 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1400 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 8.6E-04 [K^-1]
      END
    END
  END

  MATERIAL:Turpentine
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Constant Property Liquids
    PROPERTIES:
      Option = General Material
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 1.49E-03 [kg m^-1 s^-1]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1.0 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.136 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 870 [kg m^-3]
        Molar Mass = 1 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1760 [J kg^-1 K^-1]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
      THERMAL EXPANSIVITY:
        Option = Value
        Thermal Expansivity = 9.7E-04 [K^-1]
      END
    END
  END

########################################################################
# Liquids and Binary Mixtures to be used with NASA Gases 
########################################################################
#
# Constant property liquids offset from NASA gases by latent heat.
#
# Reference states are generally set to the normal boiling point.  i.e.
# the boiling temperature at 1 atm.  There are two exceptions:
#
# Water (H2Ol)           298.15 K and 3.169 kPa
#  - for backwards compatibility reasons, it was set to this in previous
#    releases
#
# Carbon Dioxide (CO2l)  298.15 K and 643.42 kPa 
#  - CO2 has no normal boiling temperature.  The 1 atm isobar is below
#    the triple point and goes through the sublimation curve
#
# Homogenous binary mixtures use Antione coefficient data.
#
# Materials are suitable for combustion & phase change (evaporation,
# condensation, boiling, etc...)
#
# References:
# ***********
# Thermodynamic data are taken from either NIST (Pure Fluids) or 
# approximations based on critical point paramters given by Poling et al.
# (reference is in the documentation).
#
# Notes from Revision Mar-30-2007
#
# If the source is said to be the 'Book', it refers to Poling et al.'s
# "The Properties of Gases and Liquids", 4th edition
#
# An Excel file exists which contains the conversions from the units given
# in the book, which are molar, to the given units, which are mass based.
#
# Some interpolation was necessary for viscosity and thermal conductivity
# values.  These are also given in the Excel file. 
#
# Reference 1 refers to 'CRC Handbook of Chemistry and Physics'
#
# Reference 2 refers to a paper by Padua, Fareleira and Calado from 1996 in the
# Journal of Chemical and Engineering Data, V 41, pages 1488 - 1494, titled
# "Density and Viscosity Measurements of 2,2,4-Trimethylpentane (Isooctane)
# from 198 K to 348 K and up to 100 MPa".
#
############################################################################

  MATERIAL: CCl4l
    Material Description = Tetrachloromethane Liquid (CCl4)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 855.53 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  349.79 [K]
        Reference Specific Enthalpy = -787788.30 [J/kg]
        Reference Specific Entropy = 1550.02 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.001369 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.103 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 153.822 [kg kmol^-1]
        Option = Value
        Density = 1584.65 [kg/m^3]
      END
    END
  END

  MATERIAL: CCl4vl
    Binary Material1 = CCl4
    Binary Material2 = CCl4l
    Material Description = Tetrachloromethane Mixture (CCl4)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 1265.632 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 4.10445*ln(10)
        Antoine Temperature Offset C = (232.148-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: CF4l
    Material Description = Tetrafluoromethane Liquid (CF4)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 905.27 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  145.11 [K]
        Reference Specific Enthalpy = -11037447.89 [J/kg]
        Reference Specific Entropy = 205.48 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.00023202 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.096294 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 88.005 [kg kmol^-1]
        Option = Value
        Density = 1603.3 [kg/m^3]
      END
    END
  END

  MATERIAL: CF4vl
    Binary Material1 = CF4
    Binary Material2 = CF4l
    Material Description = Tetrafluoromethane Mixture (CF4)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 510.595 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 3.95894*ln(10)
        Antoine Temperature Offset C = (257.2-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: CH3OHl
    Material Description = Methanol Liquid (CH4O)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2534.5 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  337.69 [K]
        Reference Specific Enthalpy = -7318982.94 [J/kg]
        Reference Specific Entropy = 4401.50 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.00054371 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.2008 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 32.042 [kg kmol^-1]
        Option = Value
        Density = 786.33 [kg/m^3]
      END
    END
  END

  MATERIAL: CH3OHvl
    Binary Material1 = CH3OH
    Binary Material2 = CH3OHl
    Material Description = Methanol Mixture (CH4O)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 1580.08 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 5.20277*ln(10)
        Antoine Temperature Offset C = (239.5-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: COl
    Material Description = Carbon Monoxide Liquid (CO)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2277.48 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  81.66 [K]
        Reference Specific Enthalpy = -4386851.48 [J/kg]
        Reference Specific Entropy = 3662.95 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.0001713 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.1399 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 28.01 [kg kmol^-1]
        Option = Value
        Density = 791.46 [kg/m^3]
      END
    END
  END

  MATERIAL: COvl
    Binary Material1 = CO
    Binary Material2 = COl
    Material Description = Carbon Monoxide Mixture (CO)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 291.743 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 3.81912*ln(10)
        Antoine Temperature Offset C = (267.996-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: CO2l
    Material Description = Carbon Dioxide Liquid (CO2)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 6467.382 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 643.42 [kPa]
        Reference Temperature =  298.15 [K]
        Reference Specific Enthalpy = -9061843.81 [J/kg]
        Reference Specific Entropy = 3671.00 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.0000570477 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.08078855 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 44.01 [kg kmol^-1]
        Option = Value
        Density = 710.5 [kg/m^3]
      END
    END
  END

  MATERIAL: CO2vl
    Binary Material1 = CO2
    Binary Material2 = CO2l
    Material Description = Carbon Dioxide Mixture (CO2)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 1301.679 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 6.81228*ln(10)
        Antoine Temperature Offset C = (269.656-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: C2H2l
    Material Description = Acetylene Liquid (C2H2)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1424.75 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  188.4 [K]
        Reference Specific Enthalpy = 7719889.22 [J/kg]
        Reference Specific Entropy = 2835.45 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.00022146 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.107273 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 26.038 [kg kmol^-1]
        Option = Value
        Density = 598.99 [kg/m^3]
      END
    END
  END

  MATERIAL: C2H2vl
    Binary Material1 = C2H2
    Binary Material2 = C2H2l
    Material Description = Acetylene Mixture (C2H2)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 528.67 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 3.67374*ln(10)
        Antoine Temperature Offset C = (228.79-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: C2H4l
    Material Description = Ethylene (Ethene) Liquid (C2H4)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2417.5 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  169.42 [K]
        Reference Specific Enthalpy = 1191333.90 [J/kg]
        Reference Specific Entropy = 4310.84 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.00017553 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.18647 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 28.054 [kg kmol^-1]
        Option = Value
        Density = 567.65 [kg/m^3]
      END
    END
  END

  MATERIAL: C2H4vl
    Binary Material1 = C2H4
    Binary Material2 = C2H4l
    Material Description = Ethylene (Ethene) Mixture (C2H4)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 596.526 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 3.91382*ln(10)
        Antoine Temperature Offset C = (256.37-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: C2H6Ol
    Material Description = Ethanol Liquid (C2H6O)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2436.56 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  351.8 [K]
        Reference Specific Enthalpy = -5856145.81 [J/kg]
        Reference Specific Entropy = 3960.07 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.001176 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.167 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 46.069 [kg kmol^-1]
        Option = Value
        Density = 785.09 [kg/m^3]
      END
    END
  END

  MATERIAL: C2H6Ovl
    Binary Material1 = C2H6O
    Binary Material2 = C2H6Ol
    Material Description = Ethanol Mixture (C2H6O)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 1648.22 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 5.33675*ln(10)
        Antoine Temperature Offset C = (230.918-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: C3H6Ol
    Material Description = Acetone Liquid (C3H6O)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2179.75 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  329.22 [K]
        Reference Specific Enthalpy = -4158519.84 [J/kg]
        Reference Specific Entropy = 3699.52 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.000308 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.171 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 58.08 [kg kmol^-1]
        Option = Value
        Density = 785.5 [kg/m^3]
      END
    END
  END

  MATERIAL: C3H6Ovl
    Binary Material1 = C3H6O
    Binary Material2 = C3H6Ol
    Material Description = Acetone Mixture (C3H6O)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 1197.01 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 4.2184*ln(10)
        Antoine Temperature Offset C = (228.06-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: C3H8l
    Material Description = Propane Liquid (C3H8)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2247.57 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  231.02 [K]
        Reference Specific Enthalpy = -2899482.63 [J/kg]
        Reference Specific Entropy = 3882.66 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.0001978 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.12939 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 44.097 [kg kmol^-1]
        Option = Value
        Density = 581.22 [kg/m^3]
      END
    END
  END

  MATERIAL: C3H8vl
    Binary Material1 = C3H8
    Binary Material2 = C3H8l
    Material Description = Propane Mixture (C3H8)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 803.997 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 3.92828*ln(10)
        Antoine Temperature Offset C = (247.04-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: C4H10l
    Material Description = N-Butane Liquid (C4H10)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2313.12 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  272.66 [K]
        Reference Specific Enthalpy = -2721211.29 [J/kg]
        Reference Specific Entropy = 3609.33 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.00020318 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.11704 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 58.123 [kg kmol^-1]
        Option = Value
        Density = 601.08 [kg/m^3]
      END
    END
  END

  MATERIAL: C4H10vl
    Binary Material1 = C4H10
    Binary Material2 = C4H10l
    Material Description = N-Butane Mixture (C4H10)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 935.773 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 3.93266*ln(10)
        Antoine Temperature Offset C = (238.789-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: I C4H10l
    Material Description = Isobutane Liquid (C4H10)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2245.11 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  261.34 [K]
        Reference Specific Enthalpy = -2747031.82 [J/kg]
        Reference Specific Entropy = 3473.82 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.00022735 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.11207 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 58.123 [kg kmol^-1]
        Option = Value
        Density = 593.65 [kg/m^3]
      END
    END
  END

  MATERIAL: I C4H10vl
    Binary Material1 = I C4H10
    Binary Material2 = I C4H10l
    Material Description = Isobutane Mixture (C4H10)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 947.54 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 4.00272*ln(10)
        Antoine Temperature Offset C = (248.87-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: C5H12l
    Material Description = N-Pentane Liquid (C5H12)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2315.22 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  309.22 [K]
        Reference Specific Enthalpy = -2367130.84 [J/kg]
        Reference Specific Entropy = 3747.94 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.0002179 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.11136 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 72.15 [kg kmol^-1]
        Option = Value
        Density = 620.83 [kg/m^3]
      END
    END
  END

  MATERIAL: C5H12vl
    Binary Material1 = C5H12
    Binary Material2 = C5H12l
    Material Description = N-Pentane Mixture (C5H12)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 1064.84 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 3.97786*ln(10)
        Antoine Temperature Offset C = (232.014-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: C6H6l
    Material Description = Benzene Liquid (C6H6)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1740.41 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  353.24 [K]
        Reference Specific Enthalpy = 732499.82 [J/kg]
        Reference Specific Entropy = 2532.34 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.0001291 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.105 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 78.114 [kg kmol^-1]
        Option = Value
        Density = 873.66 [kg/m^3]
      END
    END
  END

  MATERIAL: C6H6vl
    Binary Material1 = C6H6
    Binary Material2 = C6H6l
    Material Description = Benzene Mixture (C6H6)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 1184.24 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 3.98523*ln(10)
        Antoine Temperature Offset C = (217.572-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: C6H5OHl
    Material Description = Phenol Liquid (C6H6O)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1880.41 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  455.04 [K]
        Reference Specific Enthalpy = -1302016.51 [J/kg]
        Reference Specific Entropy = 2837.62 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.000783 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.136549 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 94.113 [kg kmol^-1]
        Option = Value
        Density = 1330.66 [kg/m^3]
      END
    END
  END

  MATERIAL: C6H5OHvl
    Binary Material1 = C6H5OH
    Binary Material2 = C6H5OHl
    Material Description = Phenol Mixture (C6H6O)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 1523.42 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 4.2696*ln(10)
        Antoine Temperature Offset C = (175.4-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: C6H12l
    Material Description = Cyclohexane Liquid (C6H12)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1812.6 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  353.93 [K]
        Reference Specific Enthalpy = -1743713.48 [J/kg]
        Reference Specific Entropy = 2764.79 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.0008847 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.12396 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 84.161 [kg kmol^-1]
        Option = Value
        Density = 773.89 [kg/m^3]
      END
    END
  END

  MATERIAL: C6H12vl
    Binary Material1 = C6H12
    Binary Material2 = C6H12l
    Material Description = Cyclohexane Mixture (C6H12)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 1182.774 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 393.002*ln(10)
        Antoine Temperature Offset C = (220.618-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: C6H14l
    Material Description = N-Hexane Liquid (C6H14)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2251.79 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  341.88 [K]
        Reference Specific Enthalpy = -2195512.41 [J/kg]
        Reference Specific Entropy = 3771.03 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.00029628 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.1262 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 86.177 [kg kmol^-1]
        Option = Value
        Density = 654.78 [kg/m^3]
      END
    END
  END

  MATERIAL: C6H14vl
    Binary Material1 = C6H14
    Binary Material2 = C6H14l
    Material Description = N-Hexane Mixture (C6H14)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 1170.875 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 4.00139*ln(10)
        Antoine Temperature Offset C = (224.317-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: I C6H14l
    Material Description = Isohexane (2-Methylpentane) Liquid (C6H14)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2235.4 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  333.4 [K]
        Reference Specific Enthalpy = -2286707.78 [J/kg]
        Reference Specific Entropy = 3647.51 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.00027281 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.10465 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 86.177 [kg kmol^-1]
        Option = Value
        Density = 648.6 [kg/m^3]
      END
    END
  END

  MATERIAL: I C6H14vl
    Binary Material1 = I C6H14
    Binary Material2 = I C6H14l
    Material Description = Isohexane (2-Methylpentane) Mixture (C6H14)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 1145.8 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 3.98322*ln(10)
        Antoine Temperature Offset C = (227.815-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: C7H8l
    Material Description = Toluene Liquid (C7H8)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1707.06 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  383.79 [K]
        Reference Specific Enthalpy = 294325.87 [J/kg]
        Reference Specific Entropy = 2859.08 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.0005603 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.131 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 92.141 [kg kmol^-1]
        Option = Value
        Density = 862.18 [kg/m^3]
      END
    END
  END

  MATERIAL: C7H8vl
    Binary Material1 = C7H8
    Binary Material2 = C7H8l
    Material Description = Toluene Mixture (C7H8)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 1327.62 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 4.05043*ln(10)
        Antoine Temperature Offset C = (217.625-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: C7H16l
    Material Description = Heptane Liquid (C7H16)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2240.49 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  371.57 [K]
        Reference Specific Enthalpy = -2058395.59 [J/kg]
        Reference Specific Entropy = 3815.22 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.00038849 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.131 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 100.204 [kg kmol^-1]
        Option = Value
        Density = 679.6 [kg/m^3]
      END
    END
  END

  MATERIAL: C7H16vl
    Binary Material1 = C7H16
    Binary Material2 = C7H16l
    Material Description = Heptane Mixture (C7H16)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 1263.909 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 4.02023*ln(10)
        Antoine Temperature Offset C = (216.432-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: C8H18l
    Material Description = Octane Liquid (C8H18)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2226.5 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  398.82 [K]
        Reference Specific Enthalpy = -1941286.45 [J/kg]
        Reference Specific Entropy = 3874.30 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.00050972 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.12445 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 114.231 [kg kmol^-1]
        Option = Value
        Density = 698.27 [kg/m^3]
      END
    END
  END

  MATERIAL: C8H18vl
    Binary Material1 = C8H18
    Binary Material2 = C8H18l
    Material Description = Octane Mixture (C8H18)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 1356.36 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 4.05075*ln(10)
        Antoine Temperature Offset C = (209.635-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: I C8H18l
    Material Description = Isooctane (2,2,4 trimethylpentane) Liquid (C8H18)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2088.3123 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  372.39 [K]
        Reference Specific Enthalpy = -2094584.81 [J/kg]
        Reference Specific Entropy = 3385.70 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.000473 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.0948 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 114.231 [kg kmol^-1]
        Option = Value
        Density = 687.85 [kg/m^3]
      END
    END
  END

  MATERIAL: I C8H18vl
    Binary Material1 = I C8H18
    Binary Material2 = I C8H18l
    Material Description = Isooctane (2,2,4 trimethylpentane) Mixture (C8H18)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 1257.85 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 3.93646*ln(10)
        Antoine Temperature Offset C = (220.767-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: C9H20l
    Material Description = N-Nonane Liquid (C9H20)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2207.6 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  423.97 [K]
        Reference Specific Enthalpy = -1831794.97 [J/kg]
        Reference Specific Entropy = 3937.58 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.00065402 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.12668 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 128.258 [kg kmol^-1]
        Option = Value
        Density = 714.09 [kg/m^3]
      END
    END
  END

  MATERIAL: C9H20vl
    Binary Material1 = C9H20
    Binary Material2 = C9H20l
    Material Description = N-Nonane Mixture (C9H20)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 1438.03 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 4.07356*ln(10)
        Antoine Temperature Offset C = (202.694-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: C10H22l
    Material Description = N-Decane Liquid (C10H22)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2192.5 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  447.3 [K]
        Reference Specific Enthalpy = -1733510.93 [J/kg]
        Reference Specific Entropy = 4013.00 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.00084812 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.12948 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 142.285 [kg kmol^-1]
        Option = Value
        Density = 726.53 [kg/m^3]
      END
    END
  END

  MATERIAL: C10H22vl
    Binary Material1 = C10H22
    Binary Material2 = C10H22l
    Material Description = N-Decane Mixture (C10H22)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 1495.17 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 4.06853*ln(10)
        Antoine Temperature Offset C = (193.858-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: C16H34l
    Material Description = Cetane (Hexadecane) Liquid (C16H34)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2214.435 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  559.98 [K]
        Reference Specific Enthalpy = -1305919.24 [J/kg]
        Reference Specific Entropy = 4391.92 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.003032 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.14 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 226.446 [kg kmol^-1]
        Option = Value
        Density = 769.94 [kg/m^3]
      END
    END
  END

  MATERIAL: C16H34vl
    Binary Material1 = C16H34
    Binary Material2 = C16H34l
    Material Description = Cetane (Hexadecane) Mixture (C16H34)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 1830.510 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 4.15357*ln(10)
        Antoine Temperature Offset C = (154.45-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: H2Ol
    Material Description = Water Liquid (H2O)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Interphase Mass Transfer, Liquid Phase Combustion, Water Data
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 4215.6 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 3.169 [kPa]
        Reference Temperature =  298.15 [K]
        Reference Specific Enthalpy = -15860961.15 [J/kg]
        Reference Specific Entropy = 2824.82 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.00028182 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.67908 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 18.02 [kg kmol^-1]
        Option = Value
        Density = 958.37 [kg/m^3]
      END
    END
  END

  MATERIAL: H2Ovl
    Binary Material1 = H2O
    Binary Material2 = H2Ol
    Material Description = Water Mixture (H2O)
    Material Group = Interphase Mass Transfer, Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 1687.54 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 5.11564*ln(10)
        Antoine Temperature Offset C = (230.23-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: NH3l
    Material Description = Amonia Liquid (NH3)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 4447.87 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  239.82 [K]
        Reference Specific Enthalpy = -3149692.62 [J/kg]
        Reference Specific Entropy = 9519.81 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.00025548 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.66568 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 17.031 [kg kmol^-1]
        Option = Value
        Density = 681.97 [kg/m^3]
      END
    END
  END

  MATERIAL: NH3vl
    Binary Material1 = NH3
    Binary Material2 = NH3l
    Material Description = Amonia Mixture (NH3)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 926.132 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 4.4854*ln(10)
        Antoine Temperature Offset C = (240.17-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: N2l
    Material Description = Nitrogen Liquid (N2)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2041.49 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  77.35 [K]
        Reference Specific Enthalpy = -428299.89 [J/kg]
        Reference Specific Entropy = 3497.26 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.00016065 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.14581 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 28.014 [kg kmol^-1]
        Option = Value
        Density = 806.08 [kg/m^3]
      END
    END
  END

  MATERIAL: N2vl
    Binary Material1 = N2
    Binary Material2 = N2l
    Material Description = Nitrogen Mixture (N2)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 255.68 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 3.61947*ln(10)
        Antoine Temperature Offset C = (266.55-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: O2l
    Material Description = Oxygen Liquid (O2)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1699.36 [J/kg/K]
        Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Pressure = 1 [atm]
        Reference Temperature =  90.17 [K]
        Reference Specific Enthalpy = -403798.48 [J/kg]
        Reference Specific Entropy = 3408.68 [J/kg/K]
      END      
      DYNAMIC VISCOSITY:
        Dynamic Viscosity = 0.00018534 [Pa s]
        Option = Value
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0 [m^-1]
      END
      ABSORPTION COEFFICIENT:
        Absorption Coefficient = 1 [m^-1]
        Option = Value
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.15256 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Molar Mass = 31.999 [kg kmol^-1]
        Option = Value
        Density = 1141.17 [kg/m^3]
      END
    END
  END

  MATERIAL: O2vl
    Binary Material1 = O2
    Binary Material2 = O2l
    Material Description = Oxygen Mixture (O2)
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    Option = Homogeneous Binary Mixture
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Antoine Enthalpic Coefficient B = 319.013 [K]*ln(10)
        Antoine Pressure Scale = 1 [bar]
        Antoine Reference State Constant A = 3.81634*ln(10)
        Antoine Temperature Offset C = (266.7-273.15) [K]
        Option = Antoine Equation
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

  MATERIAL: JetA Liquid
    Material Description = Liquid Jet-A Fuel (C12H23)
    Option = Pure Substance
    Thermodynamic State = Liquid
    Material Group = Liquid Phase Combustion
    PROPERTIES:
      Option = General Material
      EQUATION OF STATE:
        Option = Value
        Density = 780 [kg m^-3]
        Molar Mass = 167.31462 [kg kmol^-1]
      END
      DYNAMIC VISCOSITY:
        Option = Value
        Dynamic Viscosity = 1.5E-03 [kg m^-1 s^-1]
      END
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.14 [W m^-1 K^-1]
      END
      SPECIFIC HEAT CAPACITY:
        Option = NASA Format
        TEMPERATURE LIMITS:
          Lower Temperature = 273.15 [K]
          Midpoint Temperature = 550 [K]
          Upper Temperature = 550 [K]
        END
        LOWER INTERVAL COEFFICIENTS:
          NASA a1 =  1.9049613E+01 []
          NASA a2 = -1.6918532E-02 [K^-1]
          NASA a3 =  6.3022035E-04 [K^-2]
          NASA a4 = -1.3336577E-06 [K^-3]
          NASA a5 =  9.4335638E-10 [K^-4]
          NASA a6 = -4.4803964E+04 [K]
          NASA a7 = -6.7690200E+01 []
        END
        UPPER INTERVAL COEFFICIENTS:
          NASA a1 =  1.9049613E+01 []
          NASA a2 = -1.6918532E-02 [K^-1]
          NASA a3 =  6.3022035E-04 [K^-2]
          NASA a4 = -1.3336577E-06 [K^-3]
          NASA a5 =  9.4335638E-10 [K^-4]
          NASA a6 = -4.4803964E+04 [K]
          NASA a7 = -6.7690200E+01 []
        END
      END
      REFERENCE STATE:
        Option = NASA Format
        Reference Pressure = 1 [atm]
        Reference Temperature = 25 [C]
      END
      ABSORPTION COEFFICIENT:
        Option = Value
        Absorption Coefficient = 1.0 [m^-1]
      END
      REFRACTIVE INDEX:
        Option = Value
        Refractive Index = 1.0 [m m^-1]
      END
      SCATTERING COEFFICIENT:
        Option = Value
        Scattering Coefficient = 0.0 [m^-1]
      END
    END
  END

  MATERIAL: JetAvl
    Material Description = Jet-A Fuel vapour pressure curve
    Option = Homogeneous Binary Mixture
    Binary Material1 = JetA
    Binary Material2 = JetA Liquid
    Material Group = Gas Phase Combustion, Liquid Phase Combustion
    SATURATION PROPERTIES:
      Option = General
      PRESSURE:
        Option = Antoine Equation
        Antoine Pressure Scale = 1 [Pa]
        Antoine Reference State Constant A = 23.3
        Antoine Enthalpic Coefficient B = 5600 [K]
        Antoine Temperature Offset C = 25 [K]
      END
      TEMPERATURE:
        Option = Automatic
      END
    END
  END

########################################################################
# CHT Solids, Particle Solids
########################################################################

  MATERIAL:Asphalt
    Option = Pure Substance
    Thermodynamic State = Solid
    Material Group = CHT Solids, Particle Solids
    PROPERTIES:
      Option = General Material
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.062 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 2115 [kg m^-3]
        Molar Mass = 1 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 9.20E+02 [J kg^-1 K^-1]
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
    END
  END

  MATERIAL:Brick Common
    Option = Pure Substance
    Thermodynamic State = Solid
    Material Group = CHT Solids, Particle Solids
    PROPERTIES:
      Option = General Material
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.72 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 1920 [kg m^-3]
        Molar Mass = 1 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 8.35E+02 [J kg^-1 K^-1]
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
    END
  END

  MATERIAL:Brick Fireclay
    Option = Pure Substance
    Thermodynamic State = Solid
    Material Group = CHT Solids, Particle Solids
    PROPERTIES:
      Option = General Material
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 1.0 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 2645 [kg m^-3]
        Molar Mass = 1 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 9.60E+02 [J kg^-1 K^-1]
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
    END
  END

  MATERIAL:Building Board Hardwood
    Option = Pure Substance
    Thermodynamic State = Solid
    Material Group = CHT Solids, Particle Solids
    PROPERTIES:
      Option = General Material
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.16 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 720 [kg m^-3]
        Molar Mass = 1 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1.255E+03 [J kg^-1 K^-1]
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
    END
  END

  MATERIAL:Building Board Particle
    Option = Pure Substance
    Thermodynamic State = Solid
    Material Group = CHT Solids, Particle Solids
    PROPERTIES:
      Option = General Material
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.078 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 590 [kg m^-3]
        Molar Mass = 1 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1.300E+03 [J kg^-1 K^-1]
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
    END
  END

  MATERIAL:Building Board Softwood
    Option = Pure Substance
    Thermodynamic State = Solid
    Material Group = CHT Solids, Particle Solids
    PROPERTIES:
      Option = General Material
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.12 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 510 [kg m^-3]
        Molar Mass = 1 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1.380E+03 [J kg^-1 K^-1]
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
    END
  END

  MATERIAL:Concrete
    Option = Pure Substance
    Thermodynamic State = Solid
    Material Group = CHT Solids, Particle Solids
    PROPERTIES:
      Option = General Material
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 1.4 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 2300 [kg m^-3]
        Molar Mass = 1 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 8.80E+02 [J kg^-1 K^-1]
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
    END
  END

  MATERIAL:Glass Flint
    Option = Pure Substance
    Thermodynamic State = Solid
    Material Group = CHT Solids, Particle Solids
    PROPERTIES:
      Option = General Material
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.8 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 4200 [kg m^-3]
        Molar Mass = 1 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 5.00E+02 [J kg^-1 K^-1]
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
    END
  END

  MATERIAL:Glass Plate
    Option = Pure Substance
    Thermodynamic State = Solid
    Material Group = CHT Solids, Particle Solids
    PROPERTIES:
      Option = General Material
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 1.4 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 2500 [kg m^-3]
        Molar Mass = 1 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 7.50E+02 [J kg^-1 K^-1]
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
    END
  END

  MATERIAL:Glass Wool
    Option = Pure Substance
    Thermodynamic State = Solid
    Material Group = CHT Solids, Particle Solids
    PROPERTIES:
      Option = General Material
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.04 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 50 [kg m^-3]
        Molar Mass = 1 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 6.70E+02 [J kg^-1 K^-1]
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
    END
  END

  MATERIAL:Iron
    Option = Pure Substance
    Thermodynamic State = Solid
    Material Group = CHT Solids, Particle Solids
    PROPERTIES:
      Option = General Material
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 80.2 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 7870 [kg m^-3]
        Molar Mass = 55.85 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 4.47E+02 [J kg^-1 K^-1]
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
    END
  END

  MATERIAL:Nickel
    Option = Pure Substance
    Thermodynamic State = Solid
    Material Group = CHT Solids, Particle Solids
    PROPERTIES:
      Option = General Material
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 90.7 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 8903 [kg m^-3]
        Molar Mass = 58.69 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 4.44E+02 [J kg^-1 K^-1]
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
    END
  END

  MATERIAL:Polystyrene
    Option = Pure Substance
    Thermodynamic State = Solid
    Material Group = CHT Solids, Particle Solids
    PROPERTIES:
      Option = General Material
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.027 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 55 [kg m^-3]
        Molar Mass = 1 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 1.21E+03 [J kg^-1 K^-1]
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
    END
  END

  MATERIAL:Rubber
    Option = Pure Substance
    Thermodynamic State = Solid
    Material Group = CHT Solids, Particle Solids
    PROPERTIES:
      Option = General Material
      THERMAL CONDUCTIVITY:
        Option = Value
        Thermal Conductivity = 0.13 [W m^-1 K^-1]
      END
      EQUATION OF STATE:
        Density = 1100 [kg m^-3]
        Molar Mass = 1 [kg kmol^-1]
        Option = Value
      END
      SPECIFIC HEAT CAPACITY:
        Option = Value
        Specific Heat Capacity = 2.01E+03 [J kg^-1 K^-1]
      END
      REFERENCE STATE:
        Option = Specified Point
        Reference Specific Enthalpy = 0 [J/kg]
        Reference Specific Entropy = 0 [J/kg/K]
        Reference Temperature = 25 [C]
      END
    END
  END
END
