Rocket Nozzle Multi Function.
DEPARTMENT OF THE NAVY WASHINGTON D C
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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.
- Solid Propellant Rocket Engines