鹿畅
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发表时间：2025-10-25
发表刊物：推进技术
ISSN号：1001-4055
关键字：Cone column angle; Discharge chamber; Electron trajectories; Ion thruster; Magnetic field distribution; Plasma
CN号：11-1813/V
上一条：Effect of ion solvation energy on electrohydrodynamic behavior of ionic liquid droplets in electrospray thrusters
下一条：Analysis of model modification and performance characteristics of a square-wave grid system using oxygen as propellant
