Thrusters

Details Thrusters Thrusters

1987-04-13

1989-02-07

Stout, Donald E.

Power plants

Reaction motor

Liquid oxidizer

244169, F02K 942

Patent

active

048023337

ABSTRACT:
A thruster for use in a spacecraft uses vaporized propellant in its combustion chamber (110). Normally two propellants are used of the kind used for main thrusters so that two vaporization chambers are needed. Pressure valves (108, 109) are controlled by electronic means (220) to maintain current pressure.

REFERENCES:
patent: 2408111 (1946-09-01), Truax et al.
patent: 2917903 (1959-12-01), Stineman et al.
patent: 3097480 (1963-07-01), Sohn
patent: 3597923 (1971-08-01), Simon
patent: 3614026 (1971-10-01), Montanino et al.
patent: 3733816 (1973-05-01), Nash et al.

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