Missile nozzle configuration

Details Missile nozzle configuration Missile nozzle configuration

1964-04-13

1977-06-07

Hubler, Malcolm F.

Aeronautics and astronautics

Missile stabilization or trajectory control

Remote control

102 3, 244 315, 244 316, F41G 700

Patent

active

040278344

ABSTRACT:
1. In a guiding and propulsion system for a missile, the combination which comprises:

REFERENCES:
patent: 2397088 (1946-03-01), Clay
patent: 2404942 (1946-07-01), Bedford
patent: 3200586 (1965-08-01), Ernest
patent: 3205657 (1965-09-01), Tumavicus

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