Actuation system with passive compensation for transient loads

Details Actuation system with passive compensation for transient loads Actuation system with passive compensation for transient loads

1994-06-30

1997-03-04

Barefoot, Galen L.

Aeronautics and astronautics

Aircraft, steering propulsion

Fluid

244172, B64C 1502

Patent

active

056071230

ABSTRACT:
A thrust-vectoring actuation system for rocket nozzles in provided with force attenuation means in order to limit transient loads which the nozzle and associated structure experience during engine startup and shutdown.

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H 1381, Leauff et al, Pub Dec. 6, 1994 filed Mar. 14, 1991.

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