DocumentCode :
773647
Title :
Status Report Radioisotopic Propulsion Systems
Author :
Whiton, J.C.
Author_Institution :
National Aeronautics and Space Administration Marshall Space Flight Center Huntsville, Alabama
Volume :
12
Issue :
1
fYear :
1965
Firstpage :
183
Lastpage :
188
Abstract :
Preliminary analysis of radioisotopic propulsion systems indicates considerable potential for application to scientific probes provided current engineering postulations can be realized. Typical applications, as indicated by analysis to date, would be high energy space missions such as solar probes to distances of approximately 0.05 A. U. and explorer probes in deep space out to the vicinity of Saturn. In order for the full calculated potential of these systems to be realized, the engineering feasibility of problems such as lightweight tankage, superinsulation for liquid hydrogen storage for more than thirty days in space, and tank-pressure propellant feed systems will have to be demonstrated.
Keywords :
Engines; Hydrogen; Isotopes; Probes; Propulsion; Radioactive materials; Rockets; Solids; Temperature; Vehicles;
fLanguage :
English
Journal_Title :
Nuclear Science, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9499
Type :
jour
DOI :
10.1109/TNS.1965.4323512
Filename :
4323512
Link To Document :
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