solid propellant的例句大全

Energic level of NEPE solid propellant was analyzed, the effect regularity of ingredients different ratio and content on the propellant formulas standard theoretical specific impulse ( ISS) was studied.

借助电子计算机计算与分析了NEPE固体推进剂的能量水平，研究和比较了组分的含量与不同配比对推进剂配方标准理论比冲I（ss）~°值的规律性影响。

Synthetic method and stabilization of alpha-AlH_3 are reviewed. Introducing AlH_3 instead of aluminum powder in solid propellant. Theoretical specific impulse can be enhanced above 100N · s/ kg.

综述了三氢化铝晶体形态特征、α-AlH3的分子结构、合成方法及稳定化途径，在固体推进剂中用三氢化铝代替铝粉可使推进剂理论比冲可以增加100N·s/kg以上。

Temperature distribution measurement of combustion wave for solid propellant

固体推进剂燃烧波温度分布测定

The factors which affect the tensile modulus of solid composite propellant are discussed from four aspects: fillers, binder, filler/ binder interaction and processing technology, and the approaches are proposed to tailor the initial tensile modulus of composite solid propellant.

从填料、粘合剂、界面作用和工艺四个方面对影响复合固体推进剂模量的因素进行了讨论，提出了调节复合固体推进剂模量的技术途径。

In situ observations of scanning electron microscopy ( SEM) during uniaxial tensile process and swelling ratio measurements were applied to study the influences of neutral polymeric bonding agents ( NPBA) on the interfacial interactions between the polymer matrix and organic nitramine fillers in the solid propellant.

采用溶胀比测试和原位拉伸扫描电镜观测等手段，研究了中性聚合物键合剂（NPBA）对硝胺填充固体推进剂界面作用的影响。

Photoconductive thermoplastic recording system and it's usage in nondestructive testing of solid propellant coating layer

光导热塑记录系统在火药包覆质量激光全息无损检测中的应用

Structural integrity analysis for the canular solid propellant grains subjected to temperature loading

温度载荷下带筋套管形装药结构完整性分析

The paper analyses the nonsteady thrust component of solid propellant rockets in a simple and convenient way and estimates it by means of some experimental data. some referable conclusions are obtained.

本文用简便的方法分析了固体火箭推力不定常分量，并用实验数据对推力不定常分量作了估算，得到若干可供参考的结论。

Based on the solid propellant burning rate formula, a new method for the combustion time determination during the data treatment in solid rocket motor firing test was studied with a method of numerical integration and interpolation.

以固体推进剂燃速公式为基础，采用计算力学中的数值积分及插值法，并利用计算机技术，研究了用燃烧室药柱的实际肉厚，确定固体火箭发动机试验曲线中燃烧时间的新方法。

Frequency Spectrum Characteristic of Photoacoustic Wave of Thermal Damage of Homogeneous Solid Propellant

激光对均质固体推进剂热损伤的光声频谱特征

Shock Initiation and Global Calibration of Constitutive Equation in Reaction Zone for a Solid Propellant

固体推进剂冲击起爆及其反应区本构方程的整体标定研究

Study on Software of Solid Propellant Burning Rate Prediction Based on one-dimensional Steady-state Reaction Gas Flow

基于一维气相稳态反应流的燃速预估软件研究

Elimination of Toxic Materials and Solvents from Solid Propellant Components ( PP1058)^ Annual technical rept. For FY 1998

固体推进剂组分中的毒性材料和溶剂的去除/1998财年年度技术报告

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

The pasty propellant is a new kind of chemical propellant derived from solid propellant.

膏体推进剂是由固体推进剂衍变而成的一种新型化学推进剂。

Calculated research on the energetic characteristic of TN in composite solid propellant

TN在固体推进剂中能量特性的计算研究

Advance of Study of Storage Life for Rocket Composite Solid Propellant

火箭弹复合固体推进剂贮存安全性研究

It was concentrated on processes of crack surfaces slip, crack growth and friction heating of closed crack driven by sheer stress, heat conduction, decomposition of solid propellant and its interaction with the gas-phase product.

研究在压应力与剪切应力作用下闭合裂纹滑移、扩展、摩擦生热、热扩散、推进剂热分解及与气相产物相互作用。

By making numerical calculation of the model, the process and condition for hot-spot formation were discussed, from which it is concluded that friction between crack surfaces slip and crack growth can lead to formation of hot-spot in composite solid propellant.

通过模型数值计算，探讨推进剂裂纹摩擦产生高温热点的过程和条件。分析计算表明裂纹摩擦和扩展可导致推进剂形成高温热点。

Research on the data processing method of solid propellant rocket engine plume temperature

一种测量固体火箭发动机羽焰温度的数据处理方法研究