推进剂
- propellant;propellent;propulser;propulsive agent
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制造推进剂的最后操作是粘合剂的固化。
The final operation in propellant manufacture is the curing of the binder .
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GAP高能低特征信号推进剂的研究
Study on GAP Based High Energy , Low Signature Propellant
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这种方法既适用于普通的推进剂,也适用于含金属的推进剂。
The method is applicable to both metalized and conventional solid propellants .
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氧化铁可用以制出超高燃速的推进剂。
Iron oxide may be utilized in achieving propellants of ultrahigh burn rate .
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基于DSP的低温推进剂加注液位检测和信号处理系统设计
Digital Signal Processing System Design of Low-temperature Propellant Level Based on DSP
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硝酸酯增塑聚醚推进剂中PB类助剂的作用机理
Mechanism of PB aids added in nitrate plasticized propellants
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遥感FTIR光谱技术在固体推进剂羽焰测试中的应用
Application of Remote Sensing FTIR Spectrometry in Plume Test of Solid Propellant
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TG分析法研究双基推进剂的热分解反应动力学
Reaction Kinetics Research on Thermal Decomposition of DB Propellant with TG Analytical Method
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TN在固体推进剂中能量特性的计算研究
Calculated research on the energetic characteristic of TN in composite solid propellant
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超微细Cu2O对RDX/AP/HTPB推进剂组分热分解特性影响的研究
Effect of Superfine Cu 2O Powder on the Thermal Decomposition Characteristics of Components of RDX / AP / HTPB Propellants
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小功率电弧加热发动机地面试验(Ⅰ)NH3推进剂试验和分析
Ground experiment on arcjet thrusters (ⅰ) Experiment and analysis using NH_3 as propellant
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HTPB推进剂凝胶分解特性与老化性能的相关性
Relationship between gel decomposition characteristics and aging properties of HTPB propellants
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引入适当的交联剂、扩链剂及键合剂可使GAP推进剂力学性能达到较高的水平。
By adding proper crosslinking agent , chain extender and bonding agent , the mechanical properties of GAP based propellants can be tailored to a higher level .
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研究了含不同氧化剂的GAP推进剂燃烧特性,观察了其火焰结构及燃烧表面,测量了推进剂燃速与压强的关系。
The combustion characterisitics of GAP propellants containing different oxidizers are studied . Their flame structures and burning surface were observed and the burning rate-pressure relationship was measured .
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快燃物ACP在丁羟复合固体推进剂中的应用
Application of Fast-Burning Energetic Compound ACP in HTPB Composite Propellants
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PNTO在GAP推进剂燃烧中的催化特性
A Study on Catalysis Mechanism of PNTO in GAP Propellant Combustion
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纳米NiCu复合粉对AP及AP/HTPB推进剂热分解的催化作用
Catalysis of nano-NiCu composite powder on the pyrolysis of AP and AP / HTPB propellant
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结果表明,FTIR测试技术可用于固体推进剂羽流温度的非接触测试。
Results show that remote sensing FTIR testing technique can be used to gain the temperature of plume of propellants .
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DSC、甲基紫试验和失重试验研究了高燃速推进剂的热安定性。
The thermal stability of high burning rate propellant is studied by DSC , methyl violet test and weight loss test .
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HTPB复合固体推进剂非线性本构研究
Non-linear constitutive equation of HTPB composite solid propellant
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用热分析法研究了纳米金属粉(Ni、Cu和Al)对高氯酸铵(AP)以及AP/HTPB推进剂热分解的催化性能。
The decomposition behavior of ammonium perchlorate ( AP ) and AP / HTPB propellant has been investigated in the presence of nanometer metal powders by DTA .
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增加AP含量和金属添加剂中镁粉含量均有助于提高推进剂的燃速和拓宽其低压可燃极限。
The greater the contents of AP and magnesium are , the higher burning rates of the propellant and the broader flammability limit .
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铅盐在HMX推进剂中催化作用的研究
Research on catalysts of lead compounds in HMX propellants
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HTPB推进剂的击穿电场强度随体积电阻率的增加而升高,随介电常数的增加而降低。
The dielectric strength of HTPB propellant increases with increasing volume resistivity or decreasing dielectric coefficient .
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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。
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 .
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NEPE推进剂的冲击感度显著降低,摩擦感度有轻微增加;
The impact sensitivity decreases significantly and the friction sensitivity increases appreciably .
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NEPE类推进剂力学性能调节的新技术
New Technique for Tailoring the Mechanical Properties of NEPE Propellants
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TMO复合催化剂对AP推进剂燃速催化作用研究
Catalysis of TMO mixtures on combustion properties in AP propellants
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应用Euler理论的多相流体模型,建立了剩余推进剂排放气-粒两相湍流流动的数学模型;
The mathematic model of turbulent gas-particle flows of remained propellant space emission is established by applying multi-phase fluid model of Euler theory .
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通过单幅近距摄影,SEM及X射线荧光光谱实验对推进剂火焰特征,燃烧现象,熄火表面的形貌及元素成分进行了分析。
Single short distance photograph , scanning electron microscopy , X-ray fluorescence analysis were used to characterize the flame image , combustion phenomena , the quenched surface image and surface elements .