Accession Number:
ADD002822
Title:
Rocket Nozzle Multi Function.
Descriptive Note:
Patent,
Corporate Author:
DEPARTMENT OF THE NAVY WASHINGTON D C
Personal Author(s):
Report Date:
1976-04-27
Pagination or Media Count:
4.0
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:
Subject Categories:
- Solid Propellant Rocket Engines