Apparatus and method for docking spacecraft

Aeronautics and astronautics – Spacecraft – Attitude control

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244159, B64G 164

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active

049039199

ABSTRACT:
A docking apparatus for coupling two spacecraft comprises a rigid pressure vessel having an interior passage, and first and second docking ports communicating with said interior passage. The planes of the docking ports form an oblique angle with respect to each other, causing the docked spacecraft to assume a canted or inclined relationship. The cant angle eliminates mechanical interference between the adjoining structures of the docked spacecraft. Methods for carrying out docking between spacecraft are also disclosed.

REFERENCES:
patent: 1866438 (1932-07-01), Williamson
patent: 3332640 (1967-07-01), Nesheim
patent: 3401903 (1968-09-01), Bohr
patent: 3855806 (1974-12-01), Le Therisien
patent: 3910533 (1975-10-01), Cheatham
patent: 3952976 (1976-04-01), Fletcher et al.
patent: 3967462 (1976-07-01), DeJong
patent: 3987742 (1976-10-01), Boisrayon et al.
patent: 4057207 (1977-11-01), Hogan
patent: 4508296 (1985-04-01), Clark
patent: 4715566 (1987-12-01), Nobles
patent: 4728060 (1988-03-01), Cohen
Rockwell International Brochure, "Moving into Space", published Apr. 1985 (574-F-33).
K. Clausen et al., "Spacelab and its Services to Users", ESA Bulletin, No. 19, pp. 47-55 (Aug. 1979).

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