propellant的例句大全

Through two methods measuring cutoff thrust and pressure of com-bustion chamber when testing liquid propellant rocket engine on ground, cu-toff impulse as simulated altitude condition is obtained. These methods are revie-wed simply, too.

本文叙述在地面条件下试验液体火箭发动机时，通过测量发动机后效段推力与测量发动机燃烧室压力两种方法来求得模拟高空后效冲量，并对这两种方法作简单评论。

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

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。

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。

Experimental Studies on Effects of AP Content and Particle Size in NEPE Propellant

NEPE推进剂中AP含量及粒度效应实验研究

Concerning the life span of Chang'e-1, Sun introduced that some parameters such as left propellant, stability of storage battery and temperature maintaining level are all perfect.

关于嫦娥一号的寿命，孙泽洲表示，从目前情况来看，“嫦娥”推进剂余量、蓄电池稳定性、温度维持水平等参数都很好。

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。

Temperature distribution measurement of combustion wave for solid propellant

固体推进剂燃烧波温度分布测定

A Method of Calculating Percentage of Burned Mass of Low Temperature Sensitivity Coated propellant

低温感包覆药已燃质量分数的一种计算方法

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。

The Development, Design and Application of Surface Tension Propellant Management System

表面张力推进剂管理系统的发展、设计与应用

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。

Research of HTPB/ AP Composite Propellant Shock Wave Ignition

HTPB/AP复合推进剂冲击波点火实验研究

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

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

Third cosmic speed v_3 and relation between quantity of rocket propellant needed to obtain v_3 and the earth's position on its orbit

第三宇宙速度ν3及获得ν3所需的火箭推进剂量与地球在公转轨道上的位置的关系

An experimental investigation on three-dimensional effect of ignition process of propellant charge in large caliber guns

大口径火炮发射装药点火过程三维效应实验研究

The paper discusses influence of the non-dimensional throat area of the reversal nozzle for thrust termination and the angle included between the axes of reversal nozzle and rocket motor on the propellant weight for cutout.

本文讨论反喷管相对喉面、反喷管轴线倾角对关车药量的影响以及关车药量的计算方法。