Multicontact spacing control device

Aeronautics and astronautics – Spacecraft – Attitude control

Patent

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Details

244158R, 2441374, B64D 112, B64G 164

Patent

active

057251835

ABSTRACT:
Two members, such as a spacecraft and an object to be ejected from said spacecraft, are normally maintained in contact by an unlockable connecting device. In order to bring about an optimum control of the attitude of the object during its ejection, the two members contact each other by at least two pairs of complementary cylindrical surfaces having generatrixes parallel to the ejection force and which simultaneously lost contact. The cylindrical surfaces can be formed on a mast connected to the spacecraft and in a bore connected to the object.

REFERENCES:
patent: 3116895 (1964-01-01), Mitchum, Jr.
patent: 3196745 (1965-07-01), Sustrich
patent: 4067308 (1978-01-01), Anderson et al.
patent: 4257639 (1981-03-01), Stock
patent: 4632339 (1986-12-01), Yuan
patent: 5060888 (1991-10-01), Vezain et al.
patent: 5115708 (1992-05-01), Spariat et al.
patent: 5129601 (1992-07-01), Henkel
patent: 5395149 (1995-03-01), Herman et al.

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