| タイトル | Thermal analytic model of 30 cm engineering model mercury ion thruster |
| 本文（外部サイト） | http://hdl.handle.net/2060/19750011277 |
| 著者（英） | Oglebay, J. C. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1975-01-01 |
| 言語 | eng |
| 内容記述 | A lumped parameter thermal nodal network was 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 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. The analytical model along with comparisons between analytical and experimental results for the various operating conditions are presented. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 75N19349
NASA-TM-X-71680 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/190675 |
