Techniques associated with thermal-vacuum and bench testing, along with flight testing of the OAO-C spacecraft heat pipes are outlined, to show that the processes used in heat transfer design and testing are adequate for good performance evaluations. (Author)
Heat Pipe Investigations
1973
49 pages
Report
No indication
English
TIBKAT | 1973
|NTRS | 1973
|NTIS | 1972
|Analytical and experimental investigations on axially grooved aluminum-ethane heat pipe
Tema Archive | 2008
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