Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1978-05-12
1979-08-07
Barefoot, Galen L.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
244 52, 244 87, F42B 1516, F42B 1518, B64C 1512, B64C 1902
Patent
active
041635345
ABSTRACT:
A vehicle has two pairs of transversely oriented rudders and duplex nozzles; three motors pivot the rudders and nozzles for yaw, pitch and roll steering whereby each motor drives the requisite rudder(s) and pivots one or two nozzles so that thrust vector and aerodynamic steering is provided always in unison.
REFERENCES:
patent: 2621871 (1952-12-01), Robert
patent: 2639582 (1953-05-01), Pearlman
patent: 2868478 (1959-01-01), McCloughy
patent: 2991026 (1961-07-01), Nelson et al.
patent: 3142153 (1964-07-01), Hensley
patent: 3532304 (1970-10-01), Pyptiuk
Barefoot Galen L.
Vereinigte Flugtechnische Werke-Fokker GmbH
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