Aeronautics and astronautics – Spacecraft – Attitude control
Patent
1978-03-30
1980-04-01
Barefoot, Galen L.
Aeronautics and astronautics
Spacecraft
Attitude control
B64G 900
Patent
active
041958047
ABSTRACT:
A device for docking or joining large structures or vehicles in earth orbit under automatic and remote sensing and control. A thin flexible boom extending from one vehicle contacts the inner surface of a large open cone on the other as the two vehicles approach each other. The conical surface guides the boom end towards the apex where a reel for drawing in the boom engages the boom. As the boom is drawn in, and the vehicles come into close proximity, a mechanical latch is engaged for final rigidizing and securing.
REFERENCES:
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patent: 2761636 (1956-09-01), Finlay
patent: 3201065 (1965-08-01), Dunn
patent: 3389877 (1968-06-01), Huber et al.
patent: 3508723 (1970-04-01), Warren et al.
patent: 3737117 (1973-06-01), Belew
patent: 3753536 (1973-08-01), White
patent: 4083520 (1978-04-01), Rupp et al.
Hujsak Edward J.
Siden LeRoy E.
Barefoot Galen L.
Duncan John R.
General Dynamics Corporation
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