Dynamite Static Demolition of Expired Workshop in Propellant Factory
火药厂退役工房的销爆静态拆除
STUDY ON HIGH IGNITION TEMPERATURE PROPELLANT FOR CASELESS AMMUNITION
高燃点发射药作为无壳弹装药的可行性分析
For the propellant mechanism of increasing burning rate is discussed.
分析了这种推进剂能提高燃速的机理。
The nitroguanidine is added to the propellant during its mixing phase.
在推进剂的混合阶段将硝基胍加到推进剂中。
Research and Manufacturing of Seismic Charge Containing Gun Propellant
含发射药震源药柱研制
Applications of integral solid propellant rocket ramjets arc researched.
研究了整体式固体火箭冲压发动机的应用性能。
It is also used as a propellant in food aerosols and as a leak detector.
也可作为食品烟雾剂中的压缩气体和漏出物侦测器。
Linear activation energy method for predicting service life of propellant
线性活化能法预估推进剂贮存寿命研究
The Shenzhou seventh airship start the replenishment propellant in today.
神舟七号飞船于今天开始加注推进剂。
Analysis on Higher Pressure Exponent of a Certain Low Burning Propellant.
某缓燃推进剂压力指数偏高原因分析
A device containing its own propellant and driven by reaction propulsion.
包含自己的推进物并用反作用力推进的装置。
Application of Laser Holography to the Atomized Field of Liquid Propellant
激光全息摄影技术在液体发射药喷雾场测试中的应用
The final operation in propellant manufacture is the curing of the binder.
制造推进剂的最后操作是粘合剂的固化。
Geysering Effect of the Cryogenic Propellant Rocket and Restraint Research
低温推进剂火箭喷泉效应及其抑制
Experimental Study on Combustion Rules in Bore of Deterred Propellant Charge
钝感火药膛内燃烧规律的实验研究
A Study of Propellant Consumption of Impulsive Maneuvers in Space Rendezvous
空间交会中脉冲变轨燃料消耗研究
Aim To study the actual combustion law of deterred propellant charge in bore.
研究钝感火药装药膛内的实际燃烧规律。
The Method of Hazard Assessment Applied to Liquid Rocket Propellant Operation
危险评价方法及在液体火箭推进剂作业中的应用
Photoelastic Analysis of Combustion Chamber of Solid Propellant Rocket Engine
固体火箭发动机燃烧室光弹性分析
The helpful effect on propellant slosh effects was a secondary consideration.
推进剂晃动得有利性影响是一个次要得考虑因素。
Other ferrocene derivatives usable as rocket propellant burning rate modifiers.
可用作火箭推进剂燃速改性剂的其他二茂铁衍生物。
Combustion Characteristics of Smokeless XLDB Propellant at Low and High Pressure
无烟交联改性双基推进剂的高，低压燃烧特性
Research on flight scheme of solid propellant kinetic kill vehicle in boost stage
固体动能拦截器助推段飞行方案研究
The Compaction Wave Characteristics in Granular Beds of Propellant and Explosive.
火、炸药颗粒床中的压缩波特性
The main components of the solid propellant are nitrocellulose and nitroglycerin.
固体推进剂的主要成分为硝化棉和硝化甘油。
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