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Combustion instability in steel and ablative rocket chambersAblative and steel chambers effect on combustion instability in hydrogen oxygen rocket engine
Document ID
19680006175
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Goelz, R. R. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1968
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-1511
Report Number: NASA-TM-X-1511
Accession Number
68N15644
Funding Number(s)
CONTRACT_GRANT: 128-31-06-05-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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