Integrated two stage rocket

Ammunition and explosives – Pyrotechnics – Rocket

Patent

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Details

102374, F42B 414, F42B 1510

Patent

active

049247751

ABSTRACT:
A rocket system wherein a frustoconical or cylindrical casing contains fi and second rocket stages in series, with each stage having a nozzle extending in an aft direction. Each stage contains a solid rocket fuel, with the forward end of the fuel in the first stage filling and surrounding the nozzle of the second stage so that when the casing is severed along a plane aft of the second stage portion of the case the pressurized combustion products in the first stage forces the stages to separate.

REFERENCES:
patent: 3031842 (1962-05-01), Ledwith
patent: 3888079 (1975-06-01), Diesinger
patent: 4342252 (1982-08-01), Hagelberg et al.
patent: 4736583 (1988-04-01), Hudema et al.

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