Double piston rocket engine assembly

Details Double piston rocket engine assembly Double piston rocket engine assembly

1985-09-09

1988-02-02

Casaregola, Louis J.

Power plants

Reaction motor

Intermittent combustion

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

Patent

active

047221852

ABSTRACT:
A compact pulse-rocket engine assembly comprising an elongated housing containing an axially extending substantially cylindrical combustion chamber terminating in a nozzle means at one end. An opposite end of the housing contains a pair of angularly disposed charging chambers. Intermediate the charging chambers and the combustion chamber are a pair of angularly disposed piston valve means. The arrangement of the valve means provides for the injection of propellants into the combustion chamber for impingement at the same point throughout the operation of the piston valve means.

REFERENCES:
patent: 2918791 (1959-12-01), Greiner
patent: 2995008 (1961-08-01), Fox
patent: 3048969 (1962-08-01), Horner
patent: 3074231 (1963-01-01), Klein
patent: 3088406 (1963-05-01), Horner
patent: 3479818 (1969-11-01), Strobl
patent: 4258546 (1981-03-01), Stratton
patent: 4326377 (1982-04-01), Jaqua

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