Gaseous secondary injection thrust vector control device

Details Gaseous secondary injection thrust vector control device Gaseous secondary injection thrust vector control device

1982-03-25

1987-08-18

Croyle, Carlton R.

Power plants

Reaction motor

With thrust direction modifying means

23926523, 137812, 60254, F02K 100, F02K 128

Patent

active

046868240

ABSTRACT:
Apparatus for modulating the thrust vector of a rocket motor by injecting t gas into the divergent section of the rocket nozzle and modulating injection of the hot gas by varying the flow from a solid propellant gas generator by controlling its flow rate with a vortex throttling valve arrangement.

REFERENCES:
patent: 3134225 (1964-05-01), Pennington, Jr.
patent: 3195303 (1965-07-01), Widell
patent: 3228188 (1966-01-01), Sargent et al.
patent: 3270505 (1966-09-01), Crabill et al.
patent: 3285262 (1966-11-01), Ernst et al.
patent: 3300978 (1967-01-01), Pennington
patent: 3324891 (1967-06-01), Rhoades
patent: 3407828 (1968-10-01), Jones
patent: 3410291 (1968-11-01), Boothe et al.
patent: 3548598 (1970-12-01), Colombani et al.
patent: 3759039 (1973-09-01), Williams

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