Jet propulsion efflux outlets

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

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Details

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

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