Pyrolants for Variable Fuel-Flow Ducted Rockets

Pyrolants for Variable Fuel-Flow Ducted Rockets 

Self-sustaining decomposition or combustion characteristics with higher fuel concentration and lower oxidizer concentration. 

A high pressure exponent of burning rate approximately 0.7-0.9, but must be less than 1.0. 

A combustion temperature that is low enough to protect the flow-rate control valve from heat and high enough to ignite the combustible gas when air is introduced into the ramburner the combustion temperature of the gas-generating pyrolant is approximately 1400 K. 

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