Inventors:
John W. Park - Palm Beach Gardens FL
Durward B. Smith - Palm Beach Gardens FL
Paul Horn - Palm Beach Gardens FL
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F02K 995
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.