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Compatibility of Warm Gas Reaction Controls with Solid Propellant Exhaust Product Used on Ballistic Missiles
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1970 by SAE International in United States
Annotation ability available
A family of attitude controls has been developed using 2200 F gas from solid propellants to provide proportional reaction control thrusts of 13-125 lb, operating for durations from 1 to 10 minutes in a Pulse Duration Modulation (PDM) mode at 12-1/2 to 25 Hz with inlet pressures of 400 to 2800 psi. Operation in a solid propellant exhaust gas environment requires that condensable and particulate contaminants be accommodated without degrading performance. The exhaustive development program performed to successfully achieve contamination isolation is discussed.