propellant的例句大全

The military vertical mixer is the special equipment to process solid propellant of missiles.

军用立式混合机是加工固体导弹火箭推进剂的专用设备.

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A mass solid propellant.

'块状'.''燃料一块固体推进剂.

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...an enormous amount of propellant.

大量的推进剂

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Solid propellant is fuel and core part of solid rocket motor.

固体推进剂是固体火箭发动机的燃料,为其核心部分.

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...a propellant for nuclear rockets.

核火箭的燃料

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Technology for space chemical propulsion includes bipropellant propulsion, mono propellant propulsion and micro propulsion.

空间化学推进技术包括双组元推进 、 单组元推进和微推进技术.

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The dynamic burning rate parameters of solid propellant of meteorological rocket is tested out and calculated.

用该方法对气象探测火箭固体推进剂燃速特性进行了实验测定和计算.

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Safety Analysis on Truing Process of Solid Propellant by Finite Element Method

固体推进剂整形过程工艺安全性的有限元分析

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A Study on Projectile Motion in Aftereffect Period of Propellant Gas

弹丸在后效期内运动的研究

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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。

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Numerical simulation for the axial deformation of solid propellant grains under the high acceleration shock

高加速度冲击下固体推进剂药柱轴向形变的数值模拟

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Influence of some straight chain azido-nitramine on combustion properties of CMDB propellant

直链叠氮硝胺对双基推进剂燃烧性能的影响

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Applying burning-rate catalysts is one of optimal approaches to regulate burning rate of HTPB propellant.

使用燃速催化剂是调节丁羟推进剂燃速的最佳途径之一.

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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.

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The atomization mechanism of hypergolic rocket propellant and decomposition combustion at high pressure and turbulence burning of premixed reactant flow field are considered.

数值仿真模型中考虑了自燃推进剂雾化机理、高压分解燃烧和预混反应流湍流燃烧等。

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Measures usually taken in the astronautical engineering are to install baffles in the propellant fuel container.

常用的增加液体晃动阻尼的措施是在推进剂贮箱内安装防晃板.

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Based on the damage mitigating control ( DMC), this thesis focuses on the damage analysis and control of the coolant channel ligament which is treated as one of critical components for the liquid-propellant rocket engines ( LRE) during a transiting operating condition.

针对减损控制技术，本文以液体火箭发动机为研究对象，视推力室冷却夹套隔片为易损部件，在发动机的转工况过程中，对其损伤进行分析与控制研究。

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Study of oscillating combustion for solid propellant at a range of low frequencies with a h-burner

用H燃烧器研究推进剂低频振荡燃烧特性

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Thermal Decomposition Mechanism, Non-isothermal Reaction Kinetics of Bismuth Citrate and Its Catalytic Effect on Combustion of Double-base Propellant

柠檬酸铋的热分解机理、非等温反应动力学及其对双基推进剂燃烧的催化作用

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The purpose of the paper is to study the interior ballistics in nozzleless booster with solide propellant rocket ramjet engine with one dimension quasi steady equations.

采用一维准定常方法，对整体式固体火箭冲压发动机的无喷管助推器内弹道进行了计算。

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