Threshold measurement of secondary arc on solar arrays for Japanese spacecraft charging guideline
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説明
In this paper, we report about the test results on coupons made for Working Group 1 (WG1), which was established to make a Japanese guideline for spacecraft charging design. Laboratory tests were carried out with an external circuit simulating a spacecraft power system. The solar array coupon panels simulating the hot and return ends of a string circuit were tested under various combinations of string voltage and string current. We revealed that the threshold conditions for sustained arc were different in string voltage.
資料番号: AA0063997011
レポート番号: JAXA-SP-07-030
収録刊行物
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- 宇宙航空研究開発機構特別資料: 第4回宇宙環境シンポジウム講演論文集 = JAXA Special Publication: Proceedings of the 4th Spacecraft Environment Symposium
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宇宙航空研究開発機構特別資料: 第4回宇宙環境シンポジウム講演論文集 = JAXA Special Publication: Proceedings of the 4th Spacecraft Environment Symposium JAXA-SP-07-030 85-90, 2008-03-31
宇宙航空研究開発機構
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詳細情報 詳細情報について
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- CRID
- 1050292561262507776
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- NII論文ID
- 120006828965
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- NII書誌ID
- AA11984031
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- ISSN
- 1349113X
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- Web Site
- http://id.nii.ac.jp/1696/00005494/
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- 本文言語コード
- en
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- 資料種別
- conference paper
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- データソース種別
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- IRDB
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