Accession Number : ADD004580
Title : Spin Nozzle and Thrust Augmentor Mechanism.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE ARMY WASHINGTON D C
Personal Author(s) : McDermott,Joseph J
Report Date : 15 Feb 1977
Pagination or Media Count : 3
Abstract : The invention consists of a spin nozzle system for imparting a thrust to pre-spin a missile prior to launching. This system includes locating the spin nozzles within the outside diameter of the main missile motor. Also the nozzle exhaust gases are exited into the main motor exhaust cone to thereby augment the total missile thrust.
Descriptors : *Patents, *Thrust augmentor nozzles, *Spinning(Motion), *Rocket nozzles, Guided missiles, Rocket engines, Diameters, Rocket exhaust, Exhaust gases, Collecting methods, Thrust
Subject Categories : Rocket Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE