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.
Heat pipe investigations
01.08.1973
Sonstige
Keine Angabe
Englisch
TIBKAT | 1973
|NTIS | 1973
|NTIS | 1972
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