| タイトル | NEXT Thruster Component Verification Testing |
| 本文（外部サイト） | http://hdl.handle.net/2060/20080006654 |
| 著者（英） | Pinero, Luis R.; Sovey, James S. |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2007-12-01 |
| 言語 | eng |
| 内容記述 | Component testing is a critical part of thruster life validation activities under NASA s Evolutionary Xenon Thruster (NEXT) project testing. The high voltage propellant isolators were selected for design verification testing. Even though they are based on a heritage design, design changes were made because the isolators will be operated under different environmental conditions including temperature, voltage, and pressure. The life test of two NEXT isolators was therefore initiated and has accumulated more than 10,000 hr of operation. Measurements to date indicate only a negligibly small increase in leakage current. The cathode heaters were also selected for verification testing. The technology to fabricate these heaters, developed for the International Space Station plasma contactor hollow cathode assembly, was transferred to Aerojet for the fabrication of the NEXT prototype model ion thrusters. Testing the contractor-fabricated heaters is necessary to validate fabrication processes for high reliability heaters. This paper documents the status of the propellant isolator and cathode heater tests. |
| NASA分類 | Spacecraft Propulsion and Power |
| レポートNO | NASA/TM-2007-215036
E-16216
AIAA Paper-2007-5276 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/256943 |
