Rocket engine with redundant capabilities

Details Rocket engine with redundant capabilities Rocket engine with redundant capabilities

1985-10-04

1990-04-03

Stout, Donald E.

Power plants

Reaction motor

Liquid oxidizer

60260, 244135C, 244172, F02K 944

Patent

active

049129252

ABSTRACT:
A redundant rocket engine for high reliability that incorporates a single thrust chamber and its attendent hydrogen and oxygen injectors and provides a pair of independent but indentical engine systems that provide the fuel feed and cooling systems where one system remains in a standby condition until a malfunction occurs while the other system remains operative. The independent systems are comprised of all of the movable parts.

REFERENCES:
patent: 2686561 (1954-08-01), Isreeli et al.
patent: 2771130 (1956-11-01), Best Jr.
patent: 3937014 (1976-02-01), Plant
patent: 4073138 (1978-02-01), Beichel
patent: 4171615 (1979-10-01), Stewart et al.
patent: 4500268 (1985-02-01), Sundberg et al.
patent: 4553914 (1985-11-01), Noell et al.

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