Aeronautics and astronautics – Spacecraft – Attitude control
Patent
1995-08-30
1998-03-10
Grant, William
Aeronautics and astronautics
Spacecraft
Attitude control
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.
Geyer Freddy
Roux Christian
Vezain Gerard
Aerospatiale - Societe Nationale Industrielle
Grant William
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