4.3 Article

Use of a Langmuir Probe Instrument on Board a Pico-Satellite

期刊

IEEE TRANSACTIONS ON PLASMA SCIENCE
卷 45, 期 8, 页码 2007-2012

出版社

IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
DOI: 10.1109/TPS.2017.2700211

关键词

CubeSat; Langmuir probe; plasma physics; spacecraft (S/C) charging

资金

  1. Solar-Terrestrial Center of Excellence
  2. European Space Agency [4000112430/14/NL/MH]
  3. Belgian Scientific Policy Office

向作者/读者索取更多资源

The sweeping Langmuir probe instrument is a part of the payload of PICo-satellite for atmospheric and space science observations (PICASSO), an ESA in-orbit demonstrator. It includes four thin cylindrical probes whose electrical potential is swept to measure both plasma density and electron temperature together with the spacecraft (S/C) potential. PICASSO is a triple unit CubeSat of dimensions 340.5 mm x 100 mm x 100 mm. The orbit is expected to be a high inclination low-earth orbit. The main issue implied by the use of a pico-satellite platform for a Langmuir probe instrument is the limited conducting area of the S/C, which leads to S/C charging and drift of the instrument's electrical ground during the measurement. A specific measurement technique that includes the simultaneous measurement of the potential and current of different probes has been developed to retrieve consistent current-voltage characteristics that can be used to estimate the plasma parameters mentioned above.

作者

我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。

评论

主要评分

4.3
评分不足

次要评分

新颖性
-
重要性
-
科学严谨性
-
评价这篇论文

推荐

暂无数据
暂无数据