propellant combustion

A Study on Catalysis Mechanism of PNTO in GAP Propellant Combustion

PNTO在GAP推进剂燃烧中的催化特性

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The combustion gasbag projector structure is one of firing ways with extensive application foreground for shrapnel, it involves that the processes of propellant combustion, gasbag charge, and pullet dispersion.

子母弹燃气囊子弹抛撒系统是一种具有广泛应用前景的抛撒技术，它包括了抛撒药燃烧、燃气囊充气和各子弹运动的变化过程。

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Temperature distribution measurement of combustion wave for solid propellant

固体推进剂燃烧波温度分布测定

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Review of combustion instability testing research on liquid propellant rocket engine

液体火箭发动机燃烧不稳定性试验研究简述

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Combustion Research on Superfine Aluminium Powder In Ap/ HTPB Propellant

超细铝粉在Ap/HTPB推进剂中的燃烧研究

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It is considered that the combustion surface and the heat feedback of the propellant are increased by addition of ACP, leading that the increasing of burning rate of the propellant.

分析了ACP提高无烟改性双基推进剂燃速的作用机理，认为ACP可增加燃烧表面积和热量向燃烧表面积的反馈，使推进剂的燃速大增。

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A Study of Pressure Wave in Long Closed Bomb by Propellant Combustion

火药在长密闭管中燃烧的压力波研究

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Temperature distribution of combustion flame of double base propellant, composite propellant and NEPE propellant ( taking HNIW or HMX as oxidizer) were measured by using relative light intensity method.

采用相对光强度法测定了双基推进剂、复合推进剂及NEPE（氧化剂为HNIW或HMX）推进剂的燃烧火焰温度分布。

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In MPT system, the microwave resonator is the important component, which is in charge of the gas propellant's absorbing and transforming the microwave energy, just like the combustion chamber in chemical propulsion.

在MPT中，微波谐振腔是工质吸收与转换微波能量的重要场所，它的功能和化学推进的燃烧室一样。

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The combustion rate of propellant at any pressure can be obtained by one test of closed burner method, and closed burner method will be an effective tool to study new style propellant working under high pressure.

密闭燃烧器法一次测试可测出全部压强下推进剂燃速，可成为高压高燃推进剂研制的有效工具。

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Numerical Simulation and Experimental Study of Pasty Propellant and Solid Propellant Slurry Steady Combustion Behavior

膏体推进剂和固体推进剂药浆稳态燃烧研究

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The increasing of oxygen content in complexes have a significant influence on the thermal decomposition of mixture system, which approves that the idea adding carboxylic acid to the M/ triazole/ tetrazole system is reasonable for the combustion catalysis in double-base solid propellant.

配合物含氧量的增加对混合体系热分解的影响是明显的，通过将羧酸引入到Cu、Co、Ni/三唑、四唑体系来实现双基同体推进剂燃烧催化的思路合理。

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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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