| タイトル | Thermal analytical model of a 30 cm mercury ion thruster |
| 著者（英） | Oglebay, J. C. |
| 発行日 | 1975-03-01 |
| 言語 | eng |
| 内容記述 | A lumped parameter thermal nodal network has been developed for a 30 cm engineering model mercury ion thruster. The network consists of approximately 100 nodes coded in SINDA format for use on the Univac 1106/1108 computer. This model takes into account internal dissipation, radiation, and conduction as well as environmental heating. A series of tests were performed at NASA-Lewis Research Center to simulate a wide range of thermal environments on an operating 30 cm thruster, instrumented to measure the temperature distribution within the thruster. The results of these tests were used to calibrate the analytical model. Presented in this paper are a description of the analytical model along with comparisons between analytical and experimental results for the various operating conditions. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 75A26564
AIAA PAPER 75-344 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/448612 |
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