Combined warm gas fin and reaction control servo

Details Combined warm gas fin and reaction control servo Combined warm gas fin and reaction control servo

1976-10-04

1978-04-25

Pendegrass, Verlin R.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

244 322, F42B 1516, F42B 1518

Patent

active

040859096

ABSTRACT:
A combined reaction nozzle and fin control servo system to provide separate reaction and fin control of a missile for both high and low velocity flight phases. The servo system automatically provides a high gas flow rate for reaction nozzle control and a lower gas flow rate for fin control.
The servo system comprises a gas generator in communication with the reaction nozzles and fins, the flow of gas being regulated by a plurality of dual area piston actuators, control valves and a relief valve.

REFERENCES:
patent: 3286956 (1966-11-01), Nitikman
patent: 3415466 (1968-12-01), Poole, Jr.
patent: 3430536 (1969-03-01), Oelrich
patent: 3453828 (1969-07-01), Rawlings
patent: 3637167 (1972-01-01), Froning, Jr.

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