1) Micropropulsion
微推进
1.
Technology for space chemical propulsion includes bipropellant propulsion, monopropellant propulsion and micropropulsion.
空间化学推进技术包括双组元推进、单组元推进和微推进技术。
2.
The cost and risk of micropropulsion can be greatly reduced by use of MEMS technology.
将微机电系统(MEMS)技术应用于微推进系统可以降低成本,减少风险,并可满足微型航天器对性能、体积和质量等的特殊要求。
2) micro-thruster
微推进器
1.
Igniter is the most important part of MEMS solid propellant micro-thruster, and its igniting voltage and igniting reliability are mainly decided by the igniting resistance.
点火电路是MEMS固体化学微推进器中最重要的组成部分,其点火电压的大小及点火可靠性则主要取决于点火电阻。
2.
With the development of micro-satellite, the study of micro-thruster, including laser plasma micro-thruster, becomes urgent in recent years.
随着微卫星技术的发展,微推进器的研究已经越来越紧迫,而激光等离子体微推进器则正是其中的一种。
3.
The developments in thrust measuring techniques for the micro-thrusters are reviewed.
对近年来微推进器(Micro thruster)的推力测试技术和手段进行了较全面的综述,并对几种典型进行单脉冲冲量、平均推力等参数测量的推力测试系统和手段进行描述,分析各自的特点。
3) microthruster
微推进器
1.
A double wafer microthruster based on MEMS is designed and fabricated.
介绍了一种两层结构的MEMS冷气微推进器的设计和制作。
4) Micro thruster
微推进器
1.
MEMS based solid propellant micro thruster is a new type of micropropulsion system, which is required in microspacecraft for station keeping, attitude control, gravitation compensation and orbit adjust.
MEMS固体微推进器是一种新型的微推进系统,主要用于微型航天器的位置保持、姿态控制、引力补偿和轨道调整。
2.
Design, fabrication and test of the micro thruster were introduced in this thesis.
微推进器是一种基于MEMS技术的新型微推进系统,主要用于微小型航天器的位置保持、姿态控制、轨道调整等。
5) microwave propulsion
微波推进
6) minimum smoke propellant
微烟推进剂
1.
Impact and Friction Sensitivity of Minimum Smoke Propellant Based on NC and TMETN;
以NC和TMETN为基的微烟推进剂机械感度研究
2.
In order to investigate the effect of novel energetic catalysts on the combustion properties of minimum smoke propellant, the RDX-CMDB propellant samples containing various energetic composite catalysts were prepared through a solventless extrusion technique.
为研究含能催化剂对微烟推进剂燃烧性能的影响,制备了多种含复合含能催化剂的RDX-CM DB推进剂,利用靶线法测定了推进剂在不同压力下的燃速,并对测试结果进行了线性回归。
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