Thermo data file: thermo.dat
Propellant data file: propellant.dat
Computing case 1
Fixed enthalpy-pressure equilibrium - adiabatic flame temperature

Propellant composition
Code  Name                                mol    Mass (g)  Composition
513   HYDROGEN PEROXIDE (90 PC)           0.0100 100.0000   642H  586O  
Density :  1.387 g/cm^3
2 different elements
H  O  
Total mass:  100.000000 g
Enthalpy  : -6024.81 kJ/kg

9 possible gazeous species
2 possible condensed species

                       CHAMBER
Pressure (atm)   :       4.935
Temperature (K)  :    1316.202
H (kJ/kg)        :   -6024.805
U (kJ/kg)        :   -6519.973
G (kJ/kg)        :  -20246.613
S (kJ/(kg)(K)    :      10.805
M (g/mol)        :      22.101
(dLnV/dLnP)t     :    -1.00000
(dLnV/dLnT)p     :     1.00009
Cp (kJ/(kg)(K))  :     1.92818
Cv (kJ/(kg)(K))  :     1.55190
Cp/Cv            :     1.24246
Gamma            :     1.24246
Vson (m/s)       :   784.36380


Molar fractions

HO2                  2.2332e-007
H2                   6.7429e-008
H2O                  7.0781e-001
H2O2                 5.3485e-008
O                    5.7097e-008
OH                   2.4430e-005
O2                   2.9216e-001