Power plants – Combustion products used as motive fluid – Using special fuel or oxidizer
Patent
1984-08-20
1989-06-20
Nelson, Peter A.
Power plants
Combustion products used as motive fluid
Using special fuel or oxidizer
60225, 60253, F02C 320
Patent
active
048400246
ABSTRACT:
An integrated stage rocket motor arrangement provides boost and repeated throttling post boost operations, on demand, and includes an attitude control system. The rocket motor includes a plurality of casings for enclosing an initial boost motor, a post boost motor, and gas generator means for producing gases that are used for re-ignition of the post boost motor and as a motive source for the attitude control system. The boost motor and post boost motor are contained within the same enclosure but are separated by an internal bulkhead. The rocket motor has a plurality of nozzles one of which is located aft of the boost motor and another located within the internal bulkhead that separates the boost and post boost motors.
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"Solid-Staged Combustion Demonstrated," Aviation Week & Space Technology, Apr. 12, 1982, pp. 99 and 102.
"Aerojet Develops New Propulsion System to Give Re-Entry Vehicles More Power," Aviation Week & Space Technology, Apr. 1982, page unnumbered.
Morton Thiokol Inc.
Nelson Peter A.
Simmons James C.
White Gerald K.
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