NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Relationship between engine parameters and the fuel mass contained in an open cycle gas core reactorCavity diameter, reactor pressure, engine thrust, and hydrogen to uranium flow rate ratio of open cycle, gas core, reactor rocket engine
Document ID
19710024152
Document Type
Other
Authors
Ragsdale, R. G.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Publication Information
Publication: FLORIDA UNIV. RES. ON URANIUM PLASMAS AND THEIR TECHNOL. APPL. 1971
Subject Category
Nuclear Engineering
Accession Number
71N33628
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available