鹿畅
开通时间：..
最后更新时间：..
点击次数：
发布时间：2024-05-15
发表时间：2023-12-18
发表刊物：AIAA JOURNAL
卷号：61
期号：12
页面范围：5264-5276
ISSN号：0001-1452
关键字：DISCHARGE; HALL THRUSTER; PERFORMANCE; TRANSITIONS
上一条：Multi-hole grid thruster plume simulation model based on single grid aperture analytical model
下一条：Trilinear Immersed-Finite-Element Method for Three-Dimensional Anisotropic Interface Problems in Plasma Thrusters
