Multiple propellant solid rocket motor

Power plants – Combustion products used as motive fluid – Using special fuel or oxidizer

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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.

REFERENCES:
patent: 3065596 (1962-11-01), Schultz
patent: 3065598 (1962-11-01), Schultz
patent: 3171248 (1965-03-01), Cedwith
patent: 3724217 (1973-04-01), McDonald
patent: 3844118 (1974-10-01), Wilkinson
patent: 4023355 (1977-05-01), McDonald
patent: 4075832 (1978-02-01), Diesinger et al.
patent: 4357795 (1982-11-01), Bastian et al.
"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.

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