Combustion Properties of a Glued Consolidation Gun Propellant
胶黏固结发射药的燃烧性能
Particle Size Analysis of Combustion Residue of Solid Propellant
固体推进剂燃烧残渣的粒度分析
Hypergolic propellant rocket engine combustion instability studies
自燃推进剂火箭发动机燃烧不稳定性研究
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
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。
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
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
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
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
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
This deduction forms the basis of the twotemperature postulate for composite propellant combustion.
这种推理就是构成复合推进剂燃烧中两温概念的基
Adjustment on the Combustion Performance of Low Flame Temperature and Low Burning Rate Double Base Propellant
低燃速低燃温双基推进剂燃烧性能的调节
The ignition and combustion characteristics of pasty propellant are important parameters for the motor design.
膏体推进剂的点火和燃烧特性是发动机设计的重要参数。
The impact of different ammonium nitrate content on combustion products of the propellant was studied theoretically.
从理论上研究了硝酸铵对发射药燃烧产物组成的影响
Nevertheless, particle size distribute does not change with the combustion chamber pressure and propellant powder percentage.
粒子尺寸分布不随燃烧室压强和推进剂铝粉含量变化。
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