| 1. | Experimental and numerical studies on 0 . 1 kw microwave plasma thruster 微波等离子体推力器的试验与数值研究 |
| 2. | Microwave plasma thruster ( mpt ) is a new type of electro - thermal thruster 微波等离子推力器( mpt )是一种电热型推力器。 |
| 3. | The particle simulation of the plume flow exhausted from the stationary plasma thruster 稳态等离子体推进器羽流的粒子模拟 |
| 4. | Electro - microwave device of microwave plasma thruster operating under vacuum condition and its experiment 微波等离子推力器真空中工作的电微波系统及其实验 |
| 5. | Microwave plasma thruster ( mpt ) is a new studying type electro - thermal propulsive device . it has prospective application in spacecraft 微波等离子推力器( microwaveplasmathruster ? mpt )是一种新型的在研电热推进装置。 |
| 6. | Microwave plasma thruster ( mpt ) is a new type of electro - thermal thruster , which has widely applied prospect because of its high specific impulse , long lifetime , low plume contaminant and so on 微波等离子推力器( mpt )是一种新型的电热型推力器,它具有比冲高、寿命长、羽流污染小等优点,具有广阔的应用前景。 |
| 7. | With advantages of simple and reliable in structure , high isp and easy control over a wide range of thrust , pulsed plasma thruster ( ppt ) is very suitable for micro - satellite ' s orbit control and high precision attitude control 脉冲等离子体推力器( ppt )具有结构简单可靠,比冲高,推力在较大范围可控的特点,适合用于微、小卫星轨道控制和小卫星高精度姿态控制,其研究和应用得到了重视。 |
| 8. | Microwave plasma thruster ( mpt ) is studied in college of astronautics , northwestern polytechnical university and it is a new type of electro - thermal thruster . in order to study the performance of mpt more experiments must be taken , and an instant , exact and convenient system of measuring and controlling is very important in all of these experiments 西北工业大学航天学院微波等离子推力器( mpt ? microwaveplasmathruster )研究需要通过大量的试验探索mpt的各项性能,因此实时、准确、便捷的测控系统将为mpt的研制带来极大的便利,深入开展测控技术的研究十分必要。 |
| 9. | A coaxial micro - pulsed plasma thruster ( micro - ppt ) improved from the standard pulsed plasma thruster ( ppt ) is drawing attention by its advanced properties of low volume , high isp , high efficiency and stabilization . a coaxial micro - ppt using solid inert propellant teflon has been made in center for space science and applied research ( cssar ) , chinese academy of sciences 针对应用于微小卫星的电推进技术,各国争相开展相关的研究,其中一种经由传统的平行板电极ppt改进的同轴型脉冲等离子体微推进器(以下简称同轴型微ppt )由于其尺寸小、比冲高、效率高、工作可靠等特点尤其受到关注。 |