Ignition system for rocket engines

Details Ignition system for rocket engines Ignition system for rocket engines

1998-04-29

2000-07-04

Casaregola, Louis J.

Power plants

Reaction motor

Liquid oxidizer

60 39826, F02K 995

Patent

active

060820985

ABSTRACT:
An ignition system for a rocket engine which improves the reliability of engine re-ignition by supplying additional oxygen to the ignitor directly from the rocket engines main fuel/oxygen injector elements, thereby eliminating the need for a supplemental oxygen supply system.

REFERENCES:
patent: 3085393 (1963-04-01), Hamlin
patent: 3106059 (1963-10-01), Ledwith
patent: 4707982 (1987-11-01), Wagner
patent: 5456065 (1995-10-01), Dargies

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