| タイトル | LDEF transverse flat plate heat pipe experiment /S1005/ |
| 著者（英） | Robinson, G. A., Jr. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 1979-06-01 |
| 言語 | eng |
| 内容記述 | The paper describes the Transverse Flat Plate Heat Pipe Experiment. A transverse flat plate heat pipe is a thermal control device that serves the dual function of temperature control and mounting base for electronic equipment. In its ultimate application, the pipe would be a lightweight structure member that could be configured in a platform or enclosure and provide temperature control for large space structures, flight experiments, equipment, etc. The objective of the LDEF flight experiment is to evaluate the zero-g performance of a number of transverse flat plate heat pipe modules. Performance will include: (1) the pipes transport capability, (2) temperature drop, and (3) ability to maintain temperature over varying duty cycles and environments. Performance degradation, if any, will be monitored over the length of the LDEF mission. This information is necessary if heat pipes are to be considered for system designs where they offer benefits not available with other thermal control techniques, such as minimum weight penalty, long-life heat pipe/structural members. |
| NASA分類 | FLUID MECHANICS AND HEAT TRANSFER |
| レポートNO | 79A38053
AIAA PAPER 79-1077 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/426965 |
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