Sch. of Energy Sci. & Eng. Harbin Inst. of Technol. (HIT) Harbin China;
aerodynamics; aerospace propulsion; drag; electric propulsion; magnetic fields; plasma devices; plasma instability; vehicle dynamics; Earth gravitational field; aerodynamic drag; anode; central leak path; channel walls; computer control; cusped field plasma thruster; cusped magnetic field topology; dense plasma; discharge channel; efficiency 80 percent to 90 percent; electric propulsion devices; electrons; erosion mitigation; high ionization rate; hollow cathode; low altitude orbits; magnetic field lines; on-board propulsion system; plasma interaction; plasma stability; plasma thruster physical mechanism; propellant mass; residual atmosphere; satellites; spacecraft; two dimensional particle in cell simulation; Atmospheric measurements; Magnetic fields; Orbits; Plasmas; Propulsion; Satellites; Terrestrial atmosphere;
机译:低功率氩气电感耦合等离子体电热推进器的等离子体流体特性的数值研究和低功率氩气耦合耦合等离子体电热推进器
机译:推力性能,推进剂电离和外部放电等离子体推进器的推进器腐蚀
机译:螺旋等离子推进器中性注入对等离子密度分布和推力的修改
机译:各种推力等血浆推进器的物理机制研究
机译:应用磁场磁等离子体动力推进器的推力缩放
机译:宽范围检测器等离子体诱导高级CMOS BEOL工艺的充电效果
机译:在Helicon等离子体推进器中的中性注射中的等离子体密度分布和推力
机译:微脉冲等离子推进器的推力和性能研究