Accession Number : ADD002822

Title :   Rocket Nozzle Multi Function.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE NAVY WASHINGTON D C

Personal Author(s) : Schmidt,Joseph A ; Stone,W James

Report Date : 27 Apr 1976

Pagination or Media Count : 4

Abstract : The patent relates to a rocket motor assembly for a rocket motor used for towing a load or extracting an aircrew member from an aircraft. The rocket motor is formed in two separate sections, a casing portion and a unitary nozzle igniter housing portion. The nozzle and igniter housing portion has a circumferential portion that mates with the internal surface wall of the casing portion. A seal and fastener holds the housing in place whenever the rocket motor is assembled. A shackle secured to the igniter mechanism is fastened to a tow line extending to a load to be towed.

Descriptors :   *Escape systems, *Rocket engines, *Patents, Rocket engine cases, Rocket nozzles, Rocket igniters, Housings(Enclosures)

Subject Categories : Solid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE