Device for starting rocket-driven missiles

Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage

Patent

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Details

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.

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