| タイトル | Developments in TurboBrayton Technology for Low Temperature Applications |
| 著者（英） | Swift, W. L.; McCormick, J. A.; Zagarola, M. V.; Gibbon, Judy; Nellis, G. F. |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 1999-01-01
1999 |
| 言語 | eng |
| 内容記述 | A single stage reverse Brayton cryocooler using miniature high-speed turbomachines recently completed a successful space shuttle test flight demonstrating its capabilities for use in cooling the Near Infrared Camera and Multi-Object Spectrometer (NICMOS) on the Hubble Space Telescope (HST). The NICMOS CryoCooler (NCC) is designed for a cooling load of about 8 W at 65 K, and comprises a closed loop cryocooler coupled to an independent cryogenic circulating loop. Future space applications involve instruments that will require 5 mW to 200 mW of cooling at temperatures between 4 K and 10 K. This paper discusses the extension of Turbo-Brayton technology to meet these requirements. |
| NASA分類 | Energy Production and Conversion |
| レポートNO | TN-603 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/343941 |
