High voltage DC-DC converter for a pulsed plasma thruster of a nano-satellite
In nano-satellites, the pulsed plasma thruster (PPT) is a suitable electric propulsion system for orbit maintenance or attitude control due to its advantages of low mass (hundreds of grams), low power consumption (tens of Watts) and medium impulse bit (tens of μNs). The operating concept of PPT requ...
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| 格式: | Theses and Dissertations |
| 語言: | English |
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2017
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| 在線閱讀: | http://hdl.handle.net/10356/72709 |
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| 機構: | Nanyang Technological University |
| 語言: | English |