Aeronautics and astronautics – Spacecraft – Attitude control
Patent
1988-12-30
1989-08-22
Barefoot, Galen L.
Aeronautics and astronautics
Spacecraft
Attitude control
244159, 405188, 166343, B64G 164
Patent
active
048588571
ABSTRACT:
A system for docking a space vehicle 11 to a space station 12 where a connecting tunnel for in-flight transfer of personnel is required. Cooperable coupling mechanisms 51, 52 include docking rings 56, 61 on the space vehicle 11 and space station 12, respectively. The space station is provided with a tunnel structure 15, a retraction mechanism 30, and a docking ring 56 attached thereto. The vehicle coupling mechanism 52 is designed to capture the station coupling mechanism 51, arrest relative spacecraft motions while limiting loads to acceptable levels, and then realign the spacecraft for final docking and tunnel interconnection. The docking ring 61 of the space vehicle coupling mechanism is supported by linear attenuator actuator devices 63 each of which is controlled by a control system (FIG. 10) which receives loading information signals and attenuator stroke information signals from each device 63 and supplies output signals for controlling its linear actuation to attenuate impact loading or to realign the spacecraft for final docking and tunnel interconnection. Retraction mechanism 30 is used to draw the spacecraft together after initial contact and coupling. Tunnel trunnions 21, 22, 23, 25 cooperative with latches 67 on the space vehicle 11 constitute the primary structural tie between the spacecraft in final docked configuration.
REFERENCES:
patent: Re27903 (1974-01-01), Fogarty
patent: 3391881 (1968-07-01), Malty
patent: 3443773 (1969-05-01), Blumrich et al.
patent: 3459442 (1969-08-01), Deyarmett et al.
patent: 3513909 (1970-05-01), Peterman et al.
patent: 3517737 (1970-06-01), Peterson
patent: 3608848 (1971-09-01), Cantor et al.
patent: 3737117 (1973-06-01), Belew
patent: 3753536 (1973-08-01), White
patent: 4381092 (1983-04-01), Barker
patent: 4588150 (1986-05-01), Bock et al.
Lange Gregory A.
McManamen John P.
Schliesing John A.
Barefoot Galen L.
Fein Edward K.
Manning John R.
Schlorff Russell E.
The United States of America as represented by the Administrator
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