摘要(英) |
This article is meanly talks about how to design a micro satellite ion probe payload, and tested in space plasma simulation chamber. This is the first complete payload designed by ourselves. The design including payload case, circuit design, programing, measuring calibration, and testing all were being done in this nation. The ion temperature and plasma density in the space plasma simulation chamber were measured by the ion probe, the temperature was about 1675.9 ± 66.3 K, and the density was about 3.0256 ⨉ 105 ± 2.066 ⨉ 104 #cm-3, and through the calibration result, it can be prove that this system is a well tiny current measuring device. And this article also talks about how to improve the design, and hope in the future, there is a chance for us to put a high performance plasma measuring payload which is based on this design.
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參考文獻 |
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林再文,太空離子探測系統,中央大學碩士論文 2010
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