| タイトル | Spacecraft Potential Control by the Plasma Source Instrument on the POLAR Satellite |
| 著者（英） | Moore, T. E.; Craven, P. D.; Mozer, F. S.; Comfort, R. H.; Pollock, C. J.; Williamson, W. S. |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 1998-11-01 |
| 言語 | eng |
| 内容記述 | This increasingly recognized that the low-energy core plasma is a critically important part of magnetospheric plasma transport, yet this plasma cannot be accurately measured from spacecraft at potentials much different from that of the ambient plasma. In low-density regions such as the polar cap and lobes, spacecraft charge positively, excluding core ions from the spacecraft and accelerating core electrons so much that their velocities cannot be measured with any accuracy. In regions of high electron pressure and temperature, spacecraft charge negatively, excluding the ambient core electrons and accelerating the core ions so much that their velocity cannot be accurately measured. Plasma contactors have been used on a number of spacecraft operating in low-plasma-density regions to prevent charging of spacecraft to high potentials, particularly when exposed to high fluxes of energetic particles. This concern has prompted extensive studies by NASA for use of plasma contractors on the international space station where solar arrays may significantly affect the spacecraft potential. |
| NASA分類 | Spacecraft Design, Testing and Performance |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/344386 |
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