| タイトル | Loop Heat Pipe with Thermal Control Valve as a Variable Thermal Link |
| 本文（外部サイト） | http://hdl.handle.net/2060/20120014158 |
| 著者（英） | Walker, Kara; Anderson, William G.; Dussinger, Pete; Hartenstine, John |
| 著者所属（英） | Advanced Cooling Technologies, Inc. |
| 発行日 | 2012-09-01 |
| 言語 | eng |
| 内容記述 | Future lunar landers and rovers will require variable thermal links that allow for heat rejection during the lunar daytime and passively prevent heat rejection during the lunar night. During the lunar day, the thermal management system must reject the waste heat from the electronics and batteries to maintain them below the maximum acceptable temperature. During the lunar night, the heat rejection system must either be shut down or significant amounts of guard heat must be added to keep the electronics and batteries above the minimum acceptable temperature. Since guard heater power is unfavorable because it adds to system size and complexity, a variable thermal link is preferred to limit heat removal from the electronics and batteries during the long lunar night. Conventional loop heat pipes (LHPs) can provide the required variable thermal conductance, but they still consume electrical power to shut down the heat transfer. This innovation adds a thermal control valve (TCV) and a bypass line to a conventional LHP that proportionally allows vapor to flow back into the compensation chamber of the LHP. The addition of this valve can achieve completely passive thermal control of the LHP, eliminating the need for guard heaters and complex controls. |
| NASA分類 | Man/System Technology and Life Support |
| レポートNO | MFS-32915-1 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/262545 |
