Combination actuator and coolant supply for missile and rocket v

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

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Details

244 322, 244 327, 244117A, 60231, 23926517, 23926523, F42B 1002, F42B 1066

Patent

active

050728911

ABSTRACT:
The present invention relates to a strut assembly which may be selectively projected and retracted with respect to associated structure of a solid or liquid propellant rocket of missile, with such structure comprising one of, for example, a nozzle thereof or the body thereof. The invention struct may be projected either internally of the nozzle or externally of the missile body, as desired. Projection and retraction of the strut are accomplished through use of fluid actuation means, the fluid mode of means of which comprises coolant which is also directed in various locations on the inventive strut assembly to cool the strut assembly and to protect it and adjacent structures from particulate impaction, heat and thermal damage, etc.

REFERENCES:
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patent: 3140065 (1964-07-01), Alvarez-Calderon
patent: 3182450 (1965-05-01), Widell et al.
patent: 3246468 (1966-04-01), Wilhite
patent: 3465966 (1969-09-01), Fuentes et al.
patent: 3759466 (1973-09-01), Evers-Euterneck
patent: 4384694 (1983-05-01), Watanabe et al.
patent: 4867393 (1989-09-01), Faupell et al.
patent: 4903917 (1990-02-01), Peller et al.

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