| タイトル | Recent and planned developments at the Goddard Space Flight Center in thermal control technology |
| 著者（英） | Ollendorf, S. |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 1983-12-01 |
| 言語 | eng |
| 内容記述 | Thermal control technology for advanced spacecraft and space stations is presented. Results of proof of concept two phase laboratory devices indicate that large amounts of energy (1 to 2 kw) can be transported long distances (10 to 20 m) with very small temperature differences. An evolutionary test bed for advanced development of thermal technology, which provides data on components and systems for space station designs is described. Results of the STS-3 Thermal Canister Experiment show that the enclosure held simulated instruments to + or - 1 C over a wide range of thermal environments. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 84N19402 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/401438 |
