NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Some fuel loss rate and weight estimates of an open-cycle gas-core nuclear rocket engineEngine thrust, specific impulse, and uranium loss rate effects on gaseous fueled nuclear rocket engine weight
Document ID
19700016142
Document Type
Technical Memorandum (TM)
Authors
Ragsdale, R. G. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1970
Subject Category
NUCLEAR ENGINEERING
Report/Patent Number
NASA-TM-X-52775
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

NameType 19700016142.pdf STI