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Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine. 3 - Performance of first stage with inlet-feedpipe-manifold assemblyCold air performance test of scale model oxidizer pump drive turbine for M-1 engine - performance of first stage with inlet feedpipe manifold assembly
Document ID
19680006944
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Kline, J. F. (NASA Lewis Research Center Cleveland, OH, United States)
Stabe, R. G. (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-TN-D-4392
Report Number: NASA-TN-D-4392
Accession Number
68N16413
Funding Number(s)
CONTRACT_GRANT: 128-31-02-25-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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