Rocket engine assembly

Power plants – Reaction motor – Intermittent combustion

Patent

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Details

60258, 60259, 60 3979, F02K 502, F02K 700, F02K 900

Patent

active

047261846

ABSTRACT:
A compact pulse-rocket engine assembly comprising an elongated substantially cylindrical housing containing an axially extending substantially cylindrical combustion chamber which terminates at one end in a nozzle means. Within the housing at the opposite end of the combustion chamber are a pair of charging chambers. Intermediate the charging chambers and the combustion chambers are a pair of valve means which are parallel and linked together for ensuring that the valves operate in unison.

REFERENCES:
patent: 2918791 (1959-12-01), Greiner
patent: 3048969 (1962-08-01), Horner
patent: 3074231 (1963-01-01), Klein
patent: 3088406 (1963-05-01), Horner
patent: 3097483 (1963-07-01), Bixson et al.
patent: 3373769 (1968-03-01), Chaves, Jr. et al.
patent: 3479818 (1969-11-01), Strobl
patent: 4258546 (1981-03-01), Stratton
patent: 4326377 (1982-04-01), Jaqua

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