Development Status of a 3-D Electron Fluid Model for Hall Thruster Plume Simulations

Choi, Maria ; Yim, John T

关键词: BOUNDARY CONDITIONS;    ELECTRON ENERGY;    HALL THRUSTERS;    THREE DIMENSIONAL FLOW;    VACUUM CHAMBERS;    THREE DIMENSIONAL MODELS;    FINITE VOLUME METHOD;    DATA ACQUISITION;    NEAR FIELDS;    GROUND TESTS;   

RP-ID  :  GRC-E-DAA-TN57867

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

A 3-D electron fluid model has been developed as a steping stone to fully describe the electron current flow across magnetic fields inside a vacuum chamber and to provide electron flux to solar arrays for spacecraft surface charging model. A detailed description of the numerical treatment of the electric potential solver, including finite-volume formulation, implementation, and the treatment of boundary conditions, are presented in this paper. Verification tests of the model are presented.