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Hydrogen-oxygen Torch IgnitorThe hydrogen-oxygen torch igniter described herein has been successfully used for many years at various NASA Lewis Research Center rocket test facilities to provide ignition for rocket engine research hardware. This igniter is inexpensive, simple to operate, and has demonstrated very good reliability. It has been used as an ignition source for rocket engines that utilized a variety of propellant combinations; some of these engines developed up to 40,000 lb of thrust.
Document ID
19940022921
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Repas, George A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1994
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
NASA-TM-106493
NAS 1.15:106493
E-8480
Accession Number
94N27424
Funding Number(s)
PROJECT: RTOP 584-03-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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