Ram air steering system for a guided missile

Details Ram air steering system for a guided missile Ram air steering system for a guided missile

1983-01-19

1985-06-11

Blix, Trygve M.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

244 52, F41G 700, B64C 2108

Patent

active

045223572

ABSTRACT:
An opening in the nose of a missile allows entry of ram air during missile flight to a central chamber. Oppositely oriented steering jets are interconnected with the aft end of the central chamber and escaping ram air provides lateral steering thrust forces. A movable diverting means controls the direction that the escaping ram air is diverted and thereby controls the steering forces.

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patent: 3208383 (1965-09-01), Larson
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patent: 3502285 (1970-03-01), Gambill
patent: 3523662 (1970-08-01), Rawcliffe
patent: 3749334 (1973-07-01), McCorkle, Jr.
patent: 3977629 (1976-08-01), Tubeuf
patent: 4186899 (1980-02-01), Stewart, Jr.
patent: 4211378 (1980-07-01), Crepin
patent: 4328938 (1982-05-01), Reisman et al.

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