solid propellant的例句大全

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

Application of XPS and Sims to the study of combustion theory of solid propellant

表面分析技术（XPS及SIMS）在固体推进剂燃烧理论研究中的应用

Solid propellant is an important research field of military affairs and spaceflight technology.

固体推进剂是军事和航天技术的重要领域，一直为国内外研究者所重视。

The self-radiation spectrum of the combustion flame of a solid propellant was measured using a multi-wavelength pyrometer.

采用多波长高温计测量了某种固体推进剂燃烧火焰的自辐射光谱，并进行了数据处理。

Study of shear experiment of solid propellant with alterable directions

固体推进剂的变角剪切力学试验研究

A numerical simulation of internal flowfields in solid propellant rocket motor with radially slotted grain

径向开槽药柱发动机内流场数值模拟

The function of coarse-particle aluminium powder in high burning rate solid propellant

在高燃速推进剂中粗颗粒铝粉的作用

Study on azide composite solid propellant techniques

叠氮复合固体推进剂技术研究

Application of Remote Sensing FTIR Spectrometry in Plume Test of Solid Propellant

遥感FTIR光谱技术在固体推进剂羽焰测试中的应用

The storage life and its reliability of the solid propellant was analyzed by means of Monte-Carlo method.

采用Monte-Carlo法分析了某固体推进剂贮存的寿命及其可靠性问题。

Effects of components of fuel-rich boron-based solid propellant on burning rate in low pressure and explosive heat were investigated by measuring its burning rate with standard burner method and explosive heat with calorie meter of oxygen bomb.

采用推进剂静态燃速测试仪和氧弹式量热器的试验方法，研究了各组分对含硼富燃料推进剂低压燃速和爆热的影响。

A general purpose method for the interior ballistics calculations of solid propellant rockets

固体火箭发动机通用内弹道计算方法

The infrared laser plume measuring system is established to evaluate the performance of solid propellant.

为了准确评估固体推进剂的性能,研制了红外激光羽烟透过率测量系统.

The solid propellant booster weighs an additional 210 kg.

附加的固体火箭助推器重量210千克.

Extend-range solid propellant rocket motor is an important part of the hybrid base-burner-rocket extending range shell.

增程固体火箭发动机是底排 — 火箭复合增程炮弹的主要部件之一.

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。

The calculation of internal ballistics with one-dimensional and two-phase flow in solid propellant rocket motors

固体火箭发动机的一维两相流内弹道计算

A numerical calculation method of bulk relaxation modulus for solid propellant

固体推进剂体积松驰模量的数值解法

A Model for Erosive Burning of Solid Propellant Based on Statistical Theory of Turbulent Flame

根据紊流火焰统计理论所建立的固体推进剂侵蚀燃烧模型

The curing characteristics of NEPE composite solid propellant slurry were investigated by the dynamic rheological analysis ( DRA).

从推进剂药浆固化的动态流变特征出发，用DRA动态流变学方法研究了硝酸酯增塑聚醚推进剂的固化反应动力学。