Hybrid rocket system and integrated motor for use therein

Details Hybrid rocket system and integrated motor for use therein Hybrid rocket system and integrated motor for use therein

1999-04-09

2000-05-09

Casaregola, Louis J.

Power plants

Reaction motor

Solid and fluid propellant

60253, 60271, F02K 972

Patent

active

060586974

ABSTRACT:
A hybrid rocket system and motor includes an oxidant tank communicating with a combustion chamber containing a solid fuel grain. The passage from the oxidant tank to the combustion chamber is obstructed by a fill tube which fills the oxidant tank with oxidant and pressurizes it. Once the tank is full, the fill tube is displaced from the tank-chamber passage to deliver oxidant to the grain and initiate the combustion process. The motor may be an integral part of the rocket, or it may be a modular, expendable or exchangeable cartridge-type device inserted into a reusable body.

REFERENCES:
patent: 2791883 (1957-05-01), Moore et al.
patent: 2998703 (1961-09-01), Badders
patent: 3103784 (1963-09-01), Vetter et al.
patent: 3443475 (1969-05-01), Berton
patent: 3951072 (1976-04-01), Baker

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