Rocket nozzle multi function

Details Rocket nozzle multi function Rocket nozzle multi function

1974-06-10

1976-04-27

Engle, Samuel W.

Ammunition and explosives

Igniting devices and systems

89 1G, 244122AD, F42B 1356, F42B 1506

Patent

active

039526640

ABSTRACT:
A rocket motor assembly for a rocket motor utilized for towing a load or racting 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.

REFERENCES:
patent: 2644364 (1953-07-01), Nass
patent: 2751171 (1956-06-01), Martin
patent: 2805622 (1957-09-01), Canmin-Christy
patent: 3388666 (1968-06-01), Walther
patent: 3570405 (1971-03-01), Heady, Jr.
patent: 3807670 (1974-04-01), Suller
patent: 3885452 (1975-05-01), Weinstock et al.

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