Aeronautics and astronautics – Spacecraft – Attitude control
Patent
1996-07-02
1998-05-26
Grant, William
Aeronautics and astronautics
Spacecraft
Attitude control
6441374, 644158R, B64G 164
Patent
active
057554072
ABSTRACT:
The locking member of the ejector body (1) is a tensioning pin (6) extending inside a shaft (20) provided below the ejector body. The tensioning pin bears a ring (9) forming an abutment against which the releasing piston (7) comes to bear when the pyrotechnical igniter (12, 13) is triggered. The impact of the pin is attenuated at the end of its travel through the shaft by a shock absorber (10) held on the base of the shaft.
REFERENCES:
patent: 3174706 (1965-03-01), Wagner
patent: 3547375 (1970-12-01), Mackey
patent: 4067308 (1978-01-01), Anderson et al.
patent: 4625619 (1986-12-01), Ceniza
patent: 4632339 (1986-12-01), Yuan
patent: 5395149 (1995-03-01), Herman et al.
Aubret Jean-Pierre
Barriere Michel
Aerospattale Societe Nationale Industrielle
Grant William
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