Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1980-09-08
1982-12-21
Brown, David H.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
60230, 102378, F42B 1502, F42B 1512, F02K 120
Patent
active
043645305
ABSTRACT:
A modular, apogee-control package is disclosed which can be added to exisg missiles, and which will limit the apogee of the missile trajectory by implementation of thrust vector control (TVC). The package comprises a boost guidance unit, a solid rocket propellant motor, and jet vane TVC.
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Clark Keith E.
Dillinger Robert B.
Ripley-Lotee Michael J.
Beers R. F.
Brown David H.
Pritchard Kenneth G.
Skeer W. Thom
The United States of America as represented by the Secretary of
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