Control device for missile or the like

Details Control device for missile or the like Control device for missile or the like

1977-05-19

1979-03-13

Pendegrass, Verlin R.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

60230, 23926519, F42B 1330, F02K 120

Patent

active

041438370

ABSTRACT:
A spoiler control assembly for deflecting a stream of propelling gas to pass through an exhaust nozzle of a motor drive missile type device, wherein the spoiler control assembly includes at least one spoiler blade attached for joint rotation with a turning shaft mounted within the missile. The spoiler blade is positioned adjacent an end surface of the nozzle and is inclined at a predetermined acute angle relative to a plane extending directly across an opening of the nozzle, with the shaft being selectively rotated to extend a portion of the spoiler blade into the stream of propelling gas.

REFERENCES:
patent: 2694898 (1954-11-01), Stauff
patent: 2879955 (1959-03-01), Zborowski
patent: 3384325 (1968-05-01), Hermann
Flight, Solid-Propellant Motors, p. 42, Jan. 13, 1961.

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