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Analytical study of hydrogen turbopump cycles for advanced nuclear rockets Progress report, Sep. 15, 1964 - Sep. 15, 1965Hydrogen turbopump cycles for obtaining high engine inlet pressures in advanced nuclear rockets, and data on gaseous nuclear reactors and heavy gas containment
Document ID
19660004997
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Latham, T. S. (United Aircraft Corp. East Hartford, CT, United States)
Mc Lafferty, G. H. (United Aircraft Corp. East Hartford, CT, United States)
Michels, H. H. (United Aircraft Corp. East Hartford, CT, United States)
Roback, R. (United Aircraft Corp. East Hartford, CT, United States)
Date Acquired
August 3, 2013
Publication Date
September 1, 1965
Subject Category
Nuclear Engineering
Report/Patent Number
D-910093-19
NASA-CR-68988
Report Number: D-910093-19
Report Number: NASA-CR-68988
Accession Number
66N14286
Funding Number(s)
CONTRACT_GRANT: NASW-847
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYDROGEN
NUCLEAR ROCKET
TURBOPUMP
INLET PRESSURE

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