Accession Number:

ADD002798

Title:

Method of Controlling the Spin Rate of Tube Launched Rockets.

Descriptive Note:

Patent,

Corporate Author:

DEPARTMENT OF THE NAVY WASHINGTON D C

Report Date:

1976-06-22

Pagination or Media Count:

3.0

Abstract:

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.

Subject Categories:

  • Rockets

Distribution Statement:

APPROVED FOR PUBLIC RELEASE