| タイトル | Development of the Single Graded Groove high-performance heat pipe |
| 著者（英） | Holmes, H. R.; Ambrose, J. H. |
| 著者所属（英） | Lockheed Missiles and Space Co. |
| 発行日 | 1991-01-01 |
| 言語 | eng |
| 内容記述 | This paper describes the development of a new nonarterial heat pipe with a nominal transport capability of 100,000 W in. Data are presented for one-g transport capability as a function of tilt and working fluid quantity. The transport capability agrees well with theoretical predictions. The LMSC Graded Groove Heat Pipe exhibits the high throughput and excellent heat transfer characteristics of earlier arterial designs such as the LMSC Tapered Artery Heat Pipe. At the same time, it suffers none of the priming difficulties associated with the arterial designs. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 91A19259
AIAA PAPER 91-0366 |
| 権利 | Copyright |
