NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
A premixed hydrogen/oxygen catalytic igniterThe catalytic ignition of hydrogen and oxygen propellants was studied using a premixing hydrogen/oxygen injector. The premixed injector was designed to eliminate problems associated with catalytic ignition caused by poor propellant mixing in the catalyst bed. Mixture ratio, mass flow rate, and propellant inlet temperature were varied parametrically in testing, and a pulse mode life test of the igniter was conducted. The results of the tests showed that the premixed injector eliminated flame flashback in the reactor and increased the life of the igniter significantly. The results of the experimental program and a comparison with data collected in a previous program are given.
Document ID
19890015074
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Green, James M.
(Sverdrup Technology, Inc. Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1989
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-185113
NAS 1.26:185113
AIAA PAPER 89-2302
E-4787
Report Number: NASA-CR-185113
Report Number: NAS 1.26:185113
Report Number: AIAA PAPER 89-2302
Report Number: E-4787
Meeting Information
Meeting: Joint Propulsion Conference
Location: Monterey, CA, 10-14
Start Date: July 1, 1989
Sponsors: SAE, ASEE, ASME, AIAA
Accession Number
89N24445
Funding Number(s)
PROJECT: RTOP 506-42-11
CONTRACT_GRANT: NAS3-25266
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available