| タイトル | Accelerated life test of sputtering and anode deposit spalling in a small mercury ion thruster |
| 本文（外部サイト） | http://hdl.handle.net/2060/19750023137 |
| 著者（英） | Power, J. L. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1975-09-01 |
| 言語 | eng |
| 内容記述 | Tantalum and molybdenum sputtered from discharge chamber components during operation of a 5 centimeter diameter mercury ion thruster adhered much more strongly to coarsely grit blasted anode surfaces than to standard surfaces. Spalling of the sputtered coating did occur from a coarse screen anode surface but only in flakes less than a mesh unit long. The results were obtained in a 200 hour accelerated life test conducted at an elevated discharge potential of 64.6 volts. The test approximately reproduced the major sputter erosion and deposition effects that occur under normal operation but at approximately 75 times the normal rate. No discharge chamber component suffered sufficient erosion in the test to threaten its structural integrity or further serviceability. The test indicated that the use of tantalum-surfaced discharge chamber components in conjunction with a fine wire screen anode surface should cure the problems of sputter erosion and sputtered deposits spalling in long term operation of small mercury ion thrusters. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 75N31210
E-8152
NASA-TM-X-3269 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/188786 |
