1·Base on the characteristic of laser propulsion, an investigation was performed to find out the mechanism of the interaction between laser and propellant gas.
基于激光推进的工作特点，讨激光推进中激光与工质的相互作用迸行了研究。
2·As control force source, the solid propellant gas generator was used to exert lateral force for the end control and the turn of vertical launching of missiles.
利用固体燃气发生器作为控制力源对导弹进行侧向力控制、导弹的末端控制和垂直发射导弹的转弯具有重要的作用。
3·Only when the resonant cavity of microwave Plasma Thruster (MPT) is under the resonant state, the microwave energy can heat propellant gas to produce thrust efficiently.
微波等离子推力器(mpt)谐振腔只有在谐振状态下，微波能量才能被高效地用于加热工质产生推力。
4·Gel propellant is a new kind of propellant for rocket propulsion and other gas generator.
胶体推进剂是火箭推进和其它燃气发生器的新型待选推进剂。
5·Introduce the research gas test technology and its applications of hydrazine propellant both at home and abroad.
介绍了国内外肼类推进剂气体检测技术的研究水平和应用状况。
6·The general integral equations are derived for liquid and gas components of space propulsion systems with liquid propellant rocket engine.
针对采用液体推进剂火箭发动机的空间推进系统，推导了系统液路和气路的通用积分形式方程。
7·Ammonium nitrate (an) propellant used in missile's gas generator is studied for making it having a low burning temperature, clear gas and a larger adjusting rage of burning rate.
为使用于导弹燃气发生器的推进剂的燃温低、燃气清洁、燃速调节范围大，对硝酸铵(AN)推进剂进行了研究。
8·The models of the spinning induced effects upon propellant grain stress and deformation, thermodynamics and gas dynamics were set up.
给出了旋转对推进剂应力应变的影响、产生的热力学方面的影响及旋转引起的气体动力学的影响等的分析计算模型。
9·The hot gas produced by the igniter transfers heat to the propellant by convection.
点火器生成的高温燃气通过对流方式向推进剂传热。
10·It is supposed that the igniter produces hot gas only, and the hot gas transfers heat to the propellant by convection.
假设点火器的产物只有高温燃气，并且高温燃气通过对流方式向推进剂传热。