2) ion propulsion technology
离子推进技术
1.
According to the requirements of satellites, the thesis assumes the parameters of satellites and analyzes the application of ion propulsion technology which is applied to gravity field measurement satellites.
从重力场测量卫星要求出发,对卫星参数进行了假设,对重力场测量卫星采用离子推进技术的适用性进行了分析。
3) plasma propulsion
等离子体推进
1.
According to the problem that electromagnetic hydrodynamic propeller in the past is inefficient and hardly realized, this paper proposes the design that combines the plasma propulsion with exploding wires phenomenon in water medium.
针对传统水中电磁流体推进效率低、实现难的问题,将等离子体推进与水介质中爆炸丝现象相结合,研制出了实验用水中脉冲等离子体推进模型。
4) Microwave plasma propulsion
微波等离子推进
5) ion propulsion system
离子推进系统
1.
This challenging mission is enabled by an ion propulsion system.
在巡航和入轨后在轨运行阶段,黎明号都是以离子推进系统作为主推进。
6) Ion proplusion system
离子电推进系统
1.
For application of Ion proplusion system on geosynchronous satellite, several composition of Ion proplusion system were given.
以在地球静止轨道卫星平台上的应用为目标,较为系统地提出了离子电推进系统组成的几种方案,并对这几种方案进行了对比分析,便于构成应用系统时选择与裁剪。
补充资料：固液混合火箭推进剂(见火箭推进剂)
固液混合火箭推进剂(见火箭推进剂)
solid-liguid hybrid rocket propellant
guye hunhe huoiian tui)in)i固液混合火箭推进剂(s olid一Iiguid hy-brid rocket proPellant)见火箭推讲齐，}_
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条