Application of closed burner for measuring burning rate of solid rocket propellant
密闭燃烧器在固体火箭推进剂燃速测定中的应用研究
A Study on Measurement of Fuel rich Propellant Combustion Property at Low Pressure
低压下贫氧推进剂燃烧性能测试方法研究
Experiments conform that the DB propellant can fulfill the demands of the starter.
实验表明所选的双基推进剂能满足该起动器对装药的要求。
Minimize Propellant Consumption During Gyro System Unloading Process of Spacecraft
利用喷气装置卸载航天器积累角动量的最小工质损耗控制
The Research on Propellant Performance Effect To Chamber Press and Initial Velocity
火药性能对膛压及初速的影响研究
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。
After the mandrel is melted, a thin layer of alloy remains on the propellant surface.
此心轴溶化之后，在推进剂表面上留有一薄层的合金。
Some propellant droplets may not evaporate within the confines of the thrust chamber.
有些推进剂可能在推力室内并未汽化。
Safety monitor teehnology of propellant and explosive and initiating explosive device
火炸药与火工品作业的安全监控技术
This paper focuses on the advance in study on launch safety for gun propellant charge.
介绍了发射装药发射安全性研究进展。
The membrane tank is that one kind of liquid propellant of space system is broad used.
隔膜贮箱是一种空间系统应用较广泛得液体推进剂贮箱。
The propellant exhibits enhanced burn rate with the increase of input electric energy.
输入电能可以显著增加火药的燃速。
Analysis of liquid rocket propellant evaporation characteristic in natural environment
液体火箭推进剂在自然环境中蒸发特性
Design of Rocket Propellant Regeneration Equipment Based on Distributed Control System
基于集散控制系统的火箭推进剂再生装置的设计
The current situation of applying dimethyl ether as a aerosol propellant was introduced.
介绍了二甲醚作为抛射剂在国内外的应用现状。
An experimental study on the ignition and combustion characteristics of pasty propellant
膏体推进剂点火和燃烧特性的实验研究
Advance in the Research of the Analysis and Detection Technology of Hydrazines Propellant
肼类火箭推进剂分析检测技术研究进展
Effect of RDX on mechanical and combustion property of variable burning rate gun propellant
黑索今对变燃速发射药力学及燃烧性能的影响
The current situation of applying dimethyl ether as a new aerosol propellant was introduced.
摘要介绍了二甲醚作为抛射剂在国内外得应用现状。
This paper briefly introduced the separation recycling method of waste propellant and reuse.
本文简要介绍了废弃火药的分离回收方法及再利用。
PRELIMINARY INVESTIGATION ON GAS DYNAMIC RESONANCE IGNITION FOR LIQUID PROPELLANT ROCKET ENGINE
液体火箭发动机气动谐振点火初步研究
Composite propellant viscosity and mechanical properties were measured and analyzed theoretically.
测量与理论分析了复合推进剂的黏性与力学性能。
Study status and developing trend of respiratory protective equipment for liquid rocket propellant
火箭推进剂呼吸防护装备研究现状及发展趋势
Swelling and porosity of the propellant mixture became evident after 6 days at ambient temperature.
在室温下将药柱放置6天后，推进剂呈现膨胀和气孔。
A study on the gas generation regularity of end confined propellant charge with inner hole blockage
封端面内孔阻塞装药气体生成规律的研究
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