Aeronautics and astronautics – Spacecraft – Attitude control
Patent
1991-12-26
1992-06-30
Peters, Jr., Joseph F.
Aeronautics and astronautics
Spacecraft
Attitude control
294 655, 294 864, 901 30, 901 46, B64G 162
Patent
active
051256010
ABSTRACT:
A payload retention device (10) for grappling and retaining a payload (14) in docked position on a supporting structure (18) in the cargo bay of a space vehicle. The device comprises a two-fault tolerant electromagnetic grappling system comprising electromagnets (30A,30B) for attracting and grappling a grapple strike plate (20) affixed to the payload when in proximity thereto and an electromechanical latching assembly comprising a pair of independent latching subassemblies. Each subassembly comprises a set of latching pawls (29) which are driven into latching and unlatching positions relative to a grappled payload by a pair of gearmotors (40), each equipped with a ratchet clutch drive mechanism (75, 76) which is two-fault tolerant with respect to latching such that only one gearmotor of the four needs to be operational to effect a latch of the payload but is single fault tolerant with respect to release of a latched payload. Sensors (72,92,96) are included for automatically sensing the magnetic grappling of a payload and for automatically de-energizing the gearmotors (40) of the latching subassemblies when a latch condition is achieved.
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Barr Hardie R.
Ellis Christopher P.
Fein Edward K.
Miller Guy M.
Peters Jr. Joseph F.
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