Rocket in-tube spin device and rear sabot

Ordnance – Rocket launching – Having means restraining rocket from movement in launching...

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102522, 244 323, F41F 304

Patent

active

043076513

ABSTRACT:
A spin device attached to the rocket nozzle to impart a relatively large unt 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.

REFERENCES:
patent: 2835170 (1958-05-01), Kindelberger
patent: 2968245 (1961-01-01), Sutton
patent: 3009393 (1961-11-01), Lynch
patent: 3065696 (1962-11-01), Kleinguenther
patent: 3195406 (1965-07-01), Toomey
patent: 3251267 (1966-05-01), Hauser
patent: 3427921 (1969-02-01), Bode
patent: 3527137 (1970-09-01), Scanlon
patent: 4194706 (1980-03-01), Detalle

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