solid propellant
英 [ˈsɒlɪd prəˈpelənt]
美 [ˈsɑːlɪd prəˈpelənt]
网络 固体推进剂
双语例句
- Safety Analysis on Truing Process of Solid Propellant by Finite Element Method
固体推进剂整形过程工艺安全性的有限元分析 - An Analysis of Structure Integrity of Solid Propellant Grains Under Vibration Overload
固体推进剂药柱在振动载荷作用下的结构完整性分析 - Fuzzy Comprehensive Evaluation Method for Dust Explosion of Solid Propellant
固体推进剂粉尘爆炸危险性的模糊综合评价 - Experimental Research of Constitutive Relationship of DB Solid Propellant Grain
双基固体推进剂药柱本构关系的实验研究 - 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 - Solid propellant engine systems are basically less flexible in operation than liquid or hybrid propellant systems.
固体推进剂发动机系统的可调性基本上比液体或混合型的要差。 - 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准备时间。 - Thermodynamic cycle analysis on solid propellant air-turbo-rocket
固体推进剂吸气式涡轮火箭发动机的气动热力循环分析（英文）冲压式空气喷气发动机 - In the solid propellant electrothermal chemical ( SPETC) propulsion concept, it has been proved that plasma can be successfully used to optimize and control the propellant ignition process.
总结了常规火炮点火的现状，分析了固体药电热化学炮（SPETC）点火的潜在优势，并对等离子体点火过程中存在的燃速增强机理进行了讨论。 - Molecular Simulation on Mechanism of Bonding Agents in HTPB Solid Propellant Model
丁羟推进剂模型体系中键合剂作用机理的分子模拟研究 - The use of solid propellant gives the missile a longer service-life and shorter launch time compared to the liquid fuel ICBMs.
与液体燃料ICBM相比固体推进剂的使用提供给导弹一个较长的服役寿命和较短的发射时间。 - 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 - Application of Broadband CARS in Solid Propellant Combustion Field
宽带CARS在诊断固体推进剂燃烧场中的应用 - Based on modified Arrhenius formula, an integral method and a two-step regression method for storage life prediction of solid propellant are presented.
在修正的阿伦尼斯公式基础上，提出固体推进剂贮存寿命的整体预测方法和两步回归预测方法。 - Effect of potassium salt flame suppressors on the thermal decomposition behavior of the combustion catalysts used in solid propellant
含大量氯化物消焰剂的安全炸药钾盐消焰剂对推进剂催化剂热分解行为的影响 - Characterization, Prediction and Optimization of the Interfacial Adhesion of Composite Solid Propellant
复合固体推进剂界面粘结的预估、表征及优化 - The plume temperature is an important parameter, for solid propellant rocket engines and it is useful for determining the combustion process of the engine.
推进剂的羽焰温度是固体推进剂火箭发动机的重要参数，对于研究发动机内的燃烧过程具有重要价值。 - The experimental investigation of erosive burning in one lobe of the star core grain in a solid propellant rocket engine was carried out.
本文对星形内孔装药的一个单元星角内的侵蚀燃烧进行实验研究。 - Using parabolic trajectory of ballistic missile, surface to air missile with solid propellant can realize the aim of lesser weight and farther range.
地空导弹采用弹道导弹的抛物弹道技术，能够实现应用固体推进剂达到低质量远射程的目标。 - The Diesel Fuel Wax Crystallization Mechanism and the Action Mechanism of Pour Point Depression; solid propellant binder
柴油蜡晶结晶机理和降凝剂作用机理固体火箭燃料粘结剂 - The Effect of Poisson Rate on Mechanics Properties of Solid Propellant
泊松比对固体推进剂药柱力学性能的影响 - This paper presents a method of characteristic viscosity for evaluating reliability of double-base solid propellant through researching its ageing principles.
通过对双基火药柱老化规律的研究，提出了评定固体火药柱可靠性的特性粘度法。 - Research on Flaw Characteristic Extraction of UT Echo Signal and Neural Network Identification for Solid Propellant of Rocket Engine
固体火箭发动机药柱超声检测缺陷特征提取与神经网络识别研究 - 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。 - A theoretical model describing the process of the crack combustion and propagation in solid propellant was formulated.
建立了描述固体推进剂裂纹燃烧与扩展过程的数学模型。 - Studies the ignition mode of solid propellant processed with high-pressure waterjet.
研究固体推进剂在高压水射流作用下的点火模式。 - High overload test equipment ( HOTE) provides a test to analyze and evaluate the influence of overload on solid propellant rocket motor.
高过载试验装置为分析和研究过载对固体火箭发动机的影响提供了必要的实验手段。 - A detailed examination was made of energy partition in an impacted solid propellant.
对于固体推进剂受撞击后的内部能量分布情况，已经进行了详尽的研究。 - Effect of Magnesium Based Hydrogen Storage Materials on the Properties of Composite Solid Propellant
镁基储氢材料对AP/Al/HTPB复合固体推进剂性能的影响