Compatibility of Warm Gas Reaction Controls with Solid Propellant Exhaust Product Used on Ballistic Missiles Aeronutronic Div., Philco-Ford Corporation

Format:

Conference/Event

Author/Creator:

Hyman, Sheldon, author.

Conference Name:

National Aeronautic and Space Engineering and Manufacturing Meeting (1970-10-05 : Los Angeles, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1970

Summary:

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

Notes:

Vendor supplied data

Publisher Number:

700780

Access Restriction:

Restricted for use by site license