A HG-IFE-PIC model for ion thruster plume interactions

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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

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