propellants的例句大全

Simulating computation of burning rate temperature sensitivity of composite solid propellants

复合固体推进剂燃速温度敏感系数的模拟计算

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The principle and method of estimating the safe storage life of propellants using the thermal accelerating aging test.

介绍了热加速老化试验预估火药安全贮存寿命的方法原理。

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The Estimation of the Energy Efficiency of Rocket Propellants Through the Application of Values of Bond Energy of Chemical Bonds

利用化学键能评估火箭推进荆的能量特性

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The high temperature reaction centre above the burning surface of the double base propellants and its variety regulation are found.

实验发现了双基推进剂燃烧表面上方高温反应中心的存在和变化规律。

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The results showed the interface interaction of coupling agents and HMX may be hydrogen bond essentially. The analytical resits of ESCA was in good correlation with the performance of solid propellants containing the Coupling agents.

实验结果表明：偶联剂与HMX间的界面作用的实质是氢键等次价键力，ESCA分析结果与偶联剂在固体推进剂中的使用效果有较好的对应关系。

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Investigation on prediction model for storage life of HTPB propellants

HTPB推进剂贮存期预估模型研究

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Nitrogen's properties benefit applications such as heat treating atmospheres, blanketing atmospheres, propellants, pneumatics, purging and pressurizing, and analytical carrier gases.

氮的性质使许多应用受益，如热处理气氛、覆盖气氛、推进剂、气体力学、净化和加压以及分解运载气体。

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Effect of bimodal AP particle size distribution on aluminum combustion in Propellants

双级配的氧化剂粒度对推进剂中铝燃烧的影响

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New Manufacturing Technique of Oblate Spherical Propellants for Powder Loads from Waste Double-base Mortar Propellants

报废双迫药改制射钉弹用球扁药新工艺研究

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A mechanical model of the uniaxial extension of composite solid propellants is propounded in this paper.

本文提出了复合固体推进剂单向拉伸力学模型。

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Application Prospects of Interpenetrating Polymer Network Technology in Solid Propellants

互穿聚合物网络技术在固体推进剂中的应用前景

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A primary study on boron-containing bamo/ thf propellants used in integrated stage motors

整体级发动机用含硼BAMO／THF推进剂的探索研究

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The scheme involved a lunar landing vehicle that was little more than a 680-kilogram skeleton, to which a propulsion system and propellants were attached.

采用的登月飞船主体重量几乎不超过680千克，此外还附有一个推进系统和螺旋桨。

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Mechanism of influence of active groups in binder on mechanical properties of HTPB propellants bipropellant liquid apogee motor

黏合剂活性基团对HTPB推进剂力学性能的影响机制双组元液体推进剂远地点发动机

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Review of Thermal Decomposition and Combustion Properties of Azide Propellants

叠氮粘合剂推进剂热分解及燃烧性能研究综述

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Combustion Theories of Porous Solid Propellants of Ultra-high Burn Rate

多孔超高燃速推进剂的燃烧理论

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Iron oxide may be utilized in achieving propellants of ultrahigh burn rate. Test method for storage life of adhesives

氧化铁可用以制出超高燃速的推进剂。GB/T7751-1987胶粘剂贮存期的测定方法

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The results show that ferrocene derivant ( RMT) can effectively enhance burn rate of propellants and reduce its pressure exponent under high pressures;

结果表明：二茂铁衍生物（RMT）能大幅提高推进剂燃速和降低高压燃速压强指数。

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This method is feasible by comparing the simulation results with the experimental data, so it can be used to simulate the high-pressure combustion process of HAN-based liquid propellants.

通过与实验结果进行对比，验证此法可行，能够用来模拟HAN基液体推进剂的高压燃烧过程。

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This paper analyzes the effects of burning rate catalysts on the theoretical specific impulse ( ISS) and the pressure exponents of NEPE high energy solid propellants.

分析了燃速催化剂对NEPE高能固体推进剂理论比冲和燃速压强指数的影响。

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