Space probe/satellite ejection apparatus for spacecraft

Mechanical guns and projectors – Fluid pressure

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244158R, 403328, B64G 164, F41B 700

Patent

active

045549052

ABSTRACT:
An ejection apparatus (19) for spinning and propelling objects (17) for ejection from a spacecraft (11) at a desired velocity and rotational speed. The apparatus includes a launch cradle (23) on which the space object (17) to be ejected rests. The cradle (23) is rotatably supported by a central hub (37) secured to upper end of pneumatic cylinder piston shaft (25). Release mechanisms (29) consisting of a retractable pin (75) and locking lug (72) is utilized to hold the cradle and object to be ejected. The release mechanism (29) has a fixed barrier member (76) which holds the retractable pin (75) in engagement with the locking lug (72) until release by upward movement of the launch cradle (23) beyond the barrier height.

REFERENCES:
patent: 2933340 (1960-04-01), McDiarmid
patent: 3059956 (1962-10-01), Geffner
patent: 3116895 (1964-01-01), Mitchum, Jr.
patent: 3380687 (1968-04-01), Wrench et al.
patent: 3433436 (1969-03-01), Mattey
patent: 4067308 (1978-01-01), Anderson et al.
patent: 4239412 (1980-12-01), Hogan

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