Electro-mechanical guidance actuator for a missile

Details Electro-mechanical guidance actuator for a missile Electro-mechanical guidance actuator for a missile

1978-08-01

1980-07-01

Brown, David H.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

F42B 1516

Patent

active

042102987

ABSTRACT:
In flight guidance of a missile is provided by a plurality of orthogonally isposed wing panels which can be rotated by a self-centering biased torque producing lever-ball joint assembly. A plurality of solenoids, operatively positioned proximate to a rotary cam member, are individually selectively activated to engage the rotary cam member which inclines the torque producing lever-ball joint assembly and rotates the wing panels in a desired direction.

REFERENCES:
patent: 3102437 (1963-09-01), Geger
patent: 3104081 (1963-09-01), Arnett
patent: 3272124 (1966-09-01), Marsh et al.
patent: 3355130 (1967-11-01), Dell
patent: 4163534 (1979-08-01), Seeger

Affiliated with

Also associated with

Rating

Electro-mechanical guidance actuator for a missile does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Electro-mechanical guidance actuator for a missile, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Electro-mechanical guidance actuator for a missile will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-296023