Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1979-08-27
1984-02-21
Tudor, Harold J.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
60230, 23926519, 23926529, 244 52, F42B 1518
Patent
active
044325126
ABSTRACT:
A jet propulsion efflux outlet assembly for effecting control of a flight vehicle in the pitch, yaw and roll senses having a nozzle through which efflux issues, a spoiler plate with an aperture through which the issueing efflux passes, the spoiler plate being movable laterally to effect control in pitch and yaw and being rotatable for control in roll.
REFERENCES:
patent: 2481059 (1949-09-01), Africano
patent: 3013494 (1961-12-01), Chanut
patent: 3039264 (1962-06-01), Ernest
patent: 3150486 (1964-09-01), Hollstein et al.
patent: 3165889 (1965-01-01), Kershner
patent: 3200586 (1965-08-01), Ernest
patent: 3302886 (1967-02-01), Doxey
patent: 3367112 (1968-02-01), Mainhardt
patent: 3410505 (1968-11-01), Gildon et al.
patent: 4163534 (1979-08-01), Seeger
British Aerospace Public Limited Company
Tudor Harold J.
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