片语

solid-propellant cluster固体燃料火箭发动机簇

solid-propellant motor固体推进剂马达

solid-propellant suspension固体推进剂主发动机

solid-propellant rockets固体推进剂火箭

solid-propellant motors固体推进剂马达

solid-propellant missile固体推进剂导弹

Solid chemical propellant固态化学推进剂

solid composite propellant复合固体推进剂

英汉例句

• to investigate the heat transfer in the solid propellant before ignition, analyzed the meaning of fourier law and modified fourier law and pointed out their application field and criterion.

  为研究点火前固体推进剂内传热过程，分析了傅里叶定律和修正的傅里叶定律的数学物理意义及其适用范围和判断準则；

• in this paper, is developed a physical model with the ignition process taken into account, for the internal ballistics calculation of solid propellant rocket motors.

  本文根据提出的考虑点火过程的内弹道计算的物理模型，建立了数学方程。

• considering the characteristics of the plume temperature measurement of solid propellant rocket engine, a new emissivity assumption was presented.

  对于固体火箭发动机羽焰温度的测量是困难的，了解其温度分布对于研究发动机内燃烧流场的特性有重要价值。

• composite solid propellant slurry is a viscous fluid with high percentage of solid particles.

  复合固体推进剂药浆是固体粒子含量很高的粘性流体。

• the homogeneity of certified reference material is studied by acoustic emission method for composite solid propellant burning rate.

  采用声发射燃速测试方法研究了复合固体推进剂方坯燃速的均匀性。

• based on the experimental study, volume creep compliance, volume relaxation modulus and their main curves and initial void content of solid propellant are given.

  通过实验研究，给出了固体推进剂的体积蠕变柔量、体积松弛模量和材料的初始气孔率。

• the principle of the hybrid techniques is by means of less solid propellant to release the storedinert gas after heated for developing the airbag.

  混合技术的原理是使用很少量的固体推进剂将存储的惰性气体加热、释放出来，用于展开气袋。

• from the view-point of design, this paper mainly represents the new features of a solid propellant rocket engine with several long wires embedded into its grain.

  本文主要从设计的角度阐述了药柱中加入长金属丝的固体火箭发动机的一些新的特点。

• using three dimensional linear viscoelasticity finite element model, numerical simulation was performed. the deformation of solid propellant grain under axial acceleration was investigated.

  并运用三维线性粘弹性有限元模型，对离心实验过程进行了数值模拟，以确定固体推进剂药柱在轴向过载作用下的变形问题。

• based on thermal viscoelastic theory of solid propellant property of which is related to the temperature and time, the 2d model of the internal star-shaped grain was set up.

  基于固体推进剂材料特性与温度和时间相关的热粘弹性理论，为提高发动机的安全性，建立了二维星孔装药的模型。

• a laser method was used for measuring transient burning rate delay of solid propellant in oscillatory combustion.

  应用激光方法测量压力振蕩过程中的固体推进剂瞬态燃速。

• the use of the solid propellant has significantly reduced the launch preparation time.

  固体推进剂的使用已经重要地减少发射準备时间。

• the paper deduced the fluid dynamics model of spinning solid propellant rockets, and validated the fluid dynamics model by analyzing the examples, the result accord with the actual status.

  推导了一种自旋固体火箭的流体动力学模型，并通过实例对模型进行了验证计算，计算结果与实际情况基本吻合。

• the high-pressure combustion properties of nepe high-energy solid propellant were simulated and calculated by using the ga-bp neural network.

  针对计算需求，对nepe类高能固体推进剂配方进行了全新表征，提出了13个表征参数。

• on the basis of investigating on the development of solid propellant technology, the development and innovation essence in solid propellant technology was summarized.

  在分析研究现代固体推进剂技术发展的基础上，归纳总结了固体推进剂技术的发展规律及技术创新本质。

• igniter is the most important part of mems solid propellant micro-thruster, and its igniting voltage and igniting reliability are mainly decided by the igniting resistance.

  点火电路是mems固体化学微推进器中最重要的组成部分，其点火电压的大小及点火可靠性则主要取决于点火电阻。

• solid propellant motors are produced by the facilities near xian, with the lantian solid rocket motor academy being responsible for their design and development.

  固体推进剂发动机由西安附近的基地生产，该基地进行设计研制的机构被称为蓝田固体火箭发动机研究所。

• china has undertaken to research and develop composite solid propellant rocket motors since 1958.

  中国从1958年开始复合固体推进剂火箭发动机的探索和研制工作。