NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Investigation of twin-spool turbopump performance Final reportSuction pressure feed systems performance testing for predictive computer program on twin-spool turbopump
Document ID
19690026868
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Andrews, F. X.
(Aerojet-General Corp. Sacramento, CA, United States)
Bair, E. K.
(Aerojet-General Corp. Sacramento, CA, United States)
Farquhar, J.
(Aerojet-General Corp. Sacramento, CA, United States)
Harris, C. L.
(Aerojet-General Corp. Sacramento, CA, United States)
Kirk, K. G.
(Aerojet-General Corp. Sacramento, CA, United States)
Lorenc, S. A.
(Aerojet-General Corp. Sacramento, CA, United States)
Nishioka, T.
(Aerojet-General Corp. Sacramento, CA, United States)
Reynolds, T. W.
(Aerojet-General Corp. Sacramento, CA, United States)
Tsuetaki, P.
(Aerojet-General Corp. Sacramento, CA, United States)
Date Acquired
September 2, 2013
Publication Date
September 5, 1969
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-72540
AGC-9400-16
Report Number: NASA-CR-72540
Report Number: AGC-9400-16
Accession Number
69N36246
Funding Number(s)
CONTRACT_GRANT: NAS3-11231
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available