| タイトル | Design and development of integral heat pipe/thermal energy storage devices |
| 著者（英） | Richter, R.; Mahefkey, E. T. |
| 著者所属（英） | Air Force Wright Aeronautical Labs.|Jet Propulsion Lab., California Inst. of Tech. |
| 発行日 | 1981-06-01 |
| 言語 | eng |
| 内容記述 | The major design and performance test subtasks in the development of small (200 to 1,000 whr) integral heat pipe/thermal energy storage devices for use with thermally driven spacecraft cryo-coolers are described. The design of the integral heat pipe/thermal energy storage device was based on a quasi steady resistance heat transfer, lumped capacitance model. Design considerations for the heat pipe and thermal storage annuli are presented. The thermomechanical stress and insulation system design for the device are reviewed. Experimental correlations are described, as are the plans for the further development of the concept. |
| NASA分類 | FLUID MECHANICS AND HEAT TRANSFER |
| レポートNO | 81A39136
AIAA PAPER 81-1159 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/416086 |
