Method of controlling the spin rate of tube launched rockets

Details Method of controlling the spin rate of tube launched rockets Method of controlling the spin rate of tube launched rockets

1974-10-30

1976-06-22

Pendegrass, Verlin R.

Aeronautics and astronautics

Missile stabilization or trajectory control

Stabilized by rotation

244 329, F42B 1332

Patent

active

039646963

ABSTRACT:
The spin rate of a rocket missile is controlled by bevelling the inside of he leading edge of the missile fins. Altering the bevel angle controls the rate of spin. The spin rate is also controlled by sweeping back the leading edges of the fins.

REFERENCES:
patent: 2145508 (1939-01-01), Denoix
patent: 3177809 (1965-04-01), Russell-French
patent: 3333790 (1967-08-01), Durand, Jr.

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