A HG-IFE-PIC model for ion thruster plume interactions
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説明
This paper presents a new algorithm, the hybrid-grid immersed-finite-element particle-in-cell, for modeling electric propulsion plume spacecraft interactions. This algorithm is designed to handle the complex boundary condition of a real spacecraft accurately while maintaining the computational speed of a standard PIC code. Simulations are performed to study multiple-ion thruster plume spacecraft interactions.
資料番号: AA0049206057
レポート番号: JAXA-SP-05-001E
収録刊行物
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- 宇宙航空研究開発機構特別資料 = JAXA Special Publication: 9th Spacecraft Charging Technology Conference
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宇宙航空研究開発機構特別資料 = JAXA Special Publication: 9th Spacecraft Charging Technology Conference JAXA-SP-05-001E 520-528, 2005-08-01
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
- 1050855511201479040
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- NII論文ID
- 120006829534
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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/1696/00006366/
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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
- CiNii Articles