Accession Number : ADD007539

Title :   Rocket In-Tube Spin Device and Rear Sabot.

Descriptive Note : Patent Application,

Corporate Author : DEPARTMENT OF THE ARMY WASHINGTON DC

Personal Author(s) : Batson,James L ; Booker,David L

Report Date : 04 Sep 1979

Pagination or Media Count : 7

Abstract : A spin device attached to the rocket nozzle to impart a relatively large amount of spin to the rocket in a short time while the rocket is guided in a tube launcher of a rearward facing step internal configuration. The device also acts as a rear shoe or sabot for the rocket. Upon contact with the rearward facing step, the spin device separates from the rocket. The forward rocket shoes leave the guidance of the forward tube at the same instant of device separation thus providing a nontip-off rocket launch. (Author)

Descriptors :   *Patent applications, *Rocket nozzles, Launch tubes, Spinning(Motion), Spin stabilized rockets, Launching, Torque, Splines, Rocket launchers, Separation, Guidance, Rocket components

Subject Categories : Rockets

Distribution Statement : APPROVED FOR PUBLIC RELEASE