Thrust vector control actuation system

Details Thrust vector control actuation system Thrust vector control actuation system

1977-02-04

1978-12-26

Pendegrass, Verlin R.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

60230, 23926519, F02K 120

Patent

active

041312465

ABSTRACT:
Four spoiler blades are pivotally mounted at the nozzle exit end of a rocket motor with opposed pairs of said spoiler blades connected to a single control means for positioning one or the other of said opposed pairs of spoiler blades in the nozzle exit thereby to position the rocket motor responsive to the exhaust gases impacting upon the spoiler blade.

REFERENCES:
patent: 2850977 (1958-09-01), Pollak
patent: 3096049 (1963-07-01), Karasinski
patent: 3786993 (1974-01-01), Burgess et al.

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