Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Patent
1975-10-08
1979-01-23
Feinberg, Samuel
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
F42B 1332
Patent
active
041356861
ABSTRACT:
This invention relates to a device for starting a rocket-driven missile whose filght course is directed opposite the flight course of a carrier aircraft, which comprises aerodynamically-acting braking means adapted to act upon said rocket-driven missile,
REFERENCES:
patent: 3004489 (1961-10-01), Griffith et al.
patent: 3158100 (1964-11-01), Finley
patent: 3228634 (1966-01-01), Chakoian et al.
Bryan James E.
Dornier GmbH
Feinberg Samuel
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