The Cryogenic Heat Pipe (CRYOHP) Experiment has been designed to test two cryogenic heat pipes independently in a micro-gravity environment. The CRYOHP experiment is manifested for flight aboard the shuttle (STS-53) which is scheduled for launch in November, 1992. This paper presents the design of this experiment and the thermal vacuum verification test results. A correlation of the test data and the planned mission operations are also provided.
Performance of the Cryogenic Heat Pipe Experiment
Sae Technical Papers
International Conference On Environmental Systems ; 1992
1992-07-01
Aufsatz (Konferenz)
Englisch
Performance of the Cryogenic Heat Pipe Experiment
NTRS | 1992
|Prediction of cryogenic heat pipe performance
NTRS | 1977
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