Abstract
Design of a propulsion system with mini-size, high specific impulse and extremely low impulse bit is highly demanded by micro and nano spacecrafts. In this paper, a MEMS based micro colloid thruster has been developed by bulk silicon processing. The dimensions of the new thruster have been reduced considerably, which allows the micro thrusters to use a working voltage of 1-3 kV instead of 5-10 kV traditionally. The emitter of the thruster is designed to enable fine thrust control in the micro Newton range. A cantilever-based test facility is further developed to test the micro colloid thruster. Experimental results show that a thrust in the order of micro Newton can be produced by a single emitter, with a working threshold voltage as low as 1400 V. © 2004 Elsevier B.V. All rights reserved.
| Original language | English |
|---|---|
| Pages (from-to) | 168-172 |
| Journal | Sensors and Actuators, A: Physical |
| Volume | 117 |
| Issue number | 1 |
| DOIs | |
| Publication status | Published - 3 Jan 2005 |
Research Keywords
- Colloid thruster
- MEMS
- Micro propulsion
- Micro thruster
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