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High Performance Turboalternator and Associated Hardware. 1 - Design of TurboalternatorPerformance of two stage axial flow turbogenerator with gas bearing rotor support system
Document ID
19690012409
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cohen, R.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Gilroy, W. K.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Spencer, W. B.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
August 4, 2013
Publication Date
March 1, 1969
Publication Information
Publisher: NASA
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-CR-1290
PWA-3070-VOL-1
Report Number: NASA-CR-1290
Report Number: PWA-3070-VOL-1
Accession Number
69N21771
Funding Number(s)
CONTRACT_GRANT: NAS3-6013
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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