| タイトル | The NASA GSFC MEMS Colloidal Thruster |
| 本文（外部サイト） | http://hdl.handle.net/2060/20040082014 |
| 著者（英） | Norgaard, Peter C.; Cardiff, Eric H.; Chepko, Ariane B.; Jamieson, Brian G. |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 2004-01-01
2004 |
| 言語 | eng |
| 内容記述 | A number of upcoming missions require different thrust levels on the same spacecraft. A highly scaleable and efficient propulsion system would allow substantial mass savings. One type of thruster that can throttle from high to low thrust while maintaining a high specific impulse is a Micro-Electro-Mechanical System (MEMS) colloidal thruster. The NASA GSFC MEMS colloidal thruster has solved the problem of electrical breakdown to permit the integration of the electrode on top of the emitter by a novel MEMS fabrication technique. Devices have been successfully fabricated and the insulation properties have been tested to show they can support the required electric field. A computational finite element model was created and used to verify the voltage required to successfully operate the thruster. An experimental setup has been prepared to test the devices with both optical and Time-Of-Flight diagnostics. |
| NASA分類 | Spacecraft Propulsion and Power |
| 権利 | No Copyright |
