Propellant Heats of Formation, Hydrogen Atoms, Oxygen Atoms & Densities
Propellant Heat of Formation ( J / kmol ) Hydrogen Oxygen Density ( kg / m^3 )
Water
-285,830,000
2
1
997.000
Water at 373 K
-280,183,000
2
1
958.400
Water at 394 K
-278,600,000
2
1
944.000
Water at 452 K
-274,240,000
2
1
903.000
Water at 531 K
-268,310,000
2
1
848.000
Water at 624 K
-261,290,000
2
1
784.000
Steam at 373 K
-239,300,000
2
1
0.588
Steam at 394 K
-238,595,000
2
1
0.557
Steam at 452 K
-236,647,000
2
1
0.485
Steam at 531 K
-233,995,000
2
1
0.413
Steam at 624 K
-230,872,000
2
1
0.351
Hydrogen
-8,123,000
2
0
70.800

Propellant heat of formation is the amount of energy per kilomole of substance required to form the molecule in the state it is in while in the propellant tank from elemental molecules at standard conditions. A positive number means energy is required to form the molecule and it will release energy when going to the standard state of its elemental components. A negative number means energy is released when forming the molecule and it will absorb energy when going to the standard state of its elemental components. Generally the higher the number, the more reactive or volatile the substance will be. When a substance is heated, its heat of formation rises.

Water is the most commonly used propellant in large liquid fueled rockets, often in solution with hydrogen peroxide. The hotter the water, the higher its heat of formation and therefore the higher its exhaust velocity. Hydrogen in sometimes used in electrically heated engines. The propellant heat of formation is used to calculate the mix heat, which is in turn used to calculate the reactant enthalpy.

mix heat = oxidizer mix * oxidizer heat of formation + propellant mix * propellant heat of formation

reactant enthalpy = fuel molar ratio * fuel heat of formation + mixture oxidizer mix * mix heat
 
 

This is used in tripropellant rocket, pumped rocket and rocket cost.
 
 

Feedback   Free Electronic Nation Home    Rocket   GNU Free Documentation License