The patent relates to a method whereby the spin rate of a rocket missile is controlled by bevelling the inside of the 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.
Method of Controlling the Spin Rate of Tube Launched Rockets
1974
3 pages
Report
No indication
English
Online Contents | 1994
The Development of Gun Launched Rockets
NTIS | 1968
|The Development of Gun Launched Rockets
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Engineering Index Backfile | 1955
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