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Stability characterization of advanced injectors Quarterly progress reportCombustion stability design criteria for injectors using hydrogen and oxygen as propellants at high combustion chamber pressures
Document ID
19690008485
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
August 5, 2013
Publication Date
October 7, 1968
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-98341
QPR-2067-Q-5
Report Number: NASA-CR-98341
Report Number: QPR-2067-Q-5
Accession Number
69N17817
Funding Number(s)
CONTRACT_GRANT: NAS8-20672
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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