| タイトル | Development of a Self-contained Heat Rejection Module (SHRM), phase 1 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760014338 |
| 著者（英） | Fleming, M. L. |
| 著者所属（英） | Vought Corp. |
| 発行日 | 1976-02-09 |
| 言語 | eng |
| 内容記述 | The laboratory prototype test hardware and testing of the Self-Contained Heat Rejection Module are discussed. The purpose of the test was to provide operational and design experience for application to a flight prototype design. It also provided test evaluation of several of the actual components which were to be used in the flight prototype hardware. Several changes were made in the flight prototype design due to these tests including simpler line routing, relocation of remote operated valves to a position upstream of the expansion valves, and shock mounting of the compressor. The concept of heat rejection control by compressor speed reduction was verified and the liquid receiver, accumulator, remote control valves, oil separator and power source were demonstrated as acceptable. A procedure for mode changes between pumped fluid and vapor compression was developed. |
| NASA分類 | FLUID MECHANICS AND HEAT TRANSFER |
| レポートNO | 76N21426
NASA-CR-147514
T211-RP-028 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/186351 |
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