Conference Paper
In an SBIR Phase I project for AFRL, Reaction Systems completed the conceptual design of a scramjet missile ignition system using stored nitrous oxide for fuel atomization barbotage gas and/or a pilot ignition torch. Exothermically decomposing N2O to N2 and O2 can deliver over 845 kW of thermal power per pound per second of N2O flow to aid the engi?
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