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Techniques for fabricating rocket engine components containing intricate flow channels Final reportFabrication of rocket engine components with intricate internal flow channels using powder metallurgy techniques
Document ID
19690027519
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ashurst, A. N. (Battelle Memorial Inst. Columbus, OH, United States)
Goldstein, M. (Battelle Memorial Inst. Columbus, OH, United States)
Ryan, M. J. (Battelle Memorial Inst. Columbus, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1969
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-72588
Report Number: NASA-CR-72588
Accession Number
69N36897
Funding Number(s)
CONTRACT_GRANT: NAS3-11189
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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