基本释义:

固体推进剂马达

网络释义

1)solid-propellant motors,固体推进剂马达

2)solid propellant,固体推进剂

3)solid propellants,固体推进剂

4)propel motor,推进马达

5)Composite solid propellant,复合固体推进剂

6)solid rocket propellant,固体火箭推进剂

用法和例句

Hygrothermal aging life model of a composite solid propellant;

某固体推进剂湿热老化模型

Fuzzy evaluation method for synthesis sensitivity of solid propellant;

固体推进剂综合感度模糊评价法

Progress in the application of nano aluminum powder in solid propellants;

纳米铝粉在固体推进剂中的应用

Application and prospects of microencapsulation in solid propellants;

微胶囊化在固体推进剂中的应用及展望

The application prospects of IPN technique to improve the mechanical properties, technological properties and creep resistance of the solid propellants in solid pro-pellant binder curing system were summarised .

分析了互穿聚合物网络(IPN)技术的特点,综述了IPN技术在固体推进剂粘合剂固化体系中提高固体推进剂力学性能、改善加工工艺性能和增强抗蠕变性能等方面的应用前景,并概述了IPN技术在固体推进剂衬层和包覆层中的应用。

This paper presents calculating formula to diagnose stress relaxation modulus on the basis of the experiments, theoretical analysis reasoning and revisal of dynamic-static viscoelastic properties for solid propellants.

在动态与静态粘弹性力学性能实验的基础上，通过动－静态力学特性理论转换计算公式的推导、分析和修正，提出适用于固体推进剂转换计算诊断应力松弛模量的公式。

Advances on burning rate catalyzer of composite solid propellant at home and abroad;

国内外复合固体推进剂燃速催化剂研究进展

Modulus tailoring of composite solid propellant;

复合固体推进剂的模量调节

The Vague Sub cluster theory is presented for investigating the constitutive relation of the stress strain curves and the factors which affect the mechanical properties of composite solid propellant.

运用模糊群子理论对影响复合固体推进剂力学性能的因素及其单向拉伸曲线进行了分析 ,结果发现 ,推进剂的力学性能可由控制阻碍形变因素和屈服因素的主次对比来调节 ;不同的拉伸曲线对应于不同的主导控制因素。

By studying and summing up the failure physical models in common use,this paper advanced a cumulative damage-reaction theory life model to the storage and usage of solid rocket propellant,and,by calculating examples,demonstrated this model clearly.

通过对常用失效物理模型的分析和总结,提出了固体火箭推进剂贮存使用寿命的累积损伤-反应论模型,并通过算例阐释了这一模型。

By using real time holographic interferometry,the solid rocket propellant combustion process were investigated and recorded by a video camera with a shooting speed of 25 frames per second and the maximum electronic shutter speed of 1/2000 second.

本文采用实时全息法与摄像机相结合的方法来研究固体火箭推进剂的燃烧过程，记录速度为２５帧／秒，曝光快门速度最高可达１／２０００秒。

Anti-stick coatings for stripping of solid rocket propellant, which could be cured at room temperature had been successfully developed.

开发一种用于固体火箭推进剂脱模的可常温固化溶剂型防粘涂料,该涂料是以常温固化型氟树脂为基体,加入改性微粉及其他各种助剂,配制而成的悬浮液。

Application Progress of Metal Fuels in Solid Propellants

金属燃料在固体推进剂中的应用进展

Study on Curing System of Four-components HTPB Composite Propellants;

丁羟四组元复合固体推进剂固化体系研究

SPIRBM (Solid Propellant Intermediate Range Ballistic Missile)

固体推进剂中程弹道导弹

A mass of solid propellant.

块状燃料一块固体推进剂

Research on the Micro-mechanics and Constitutive Relation for Solid Propellant;

固体推进剂细观力学与本构关系研究

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

Research on Two-Parameter Fracture Criterion of Composite Solid Propellants

复合固体推进剂双参数断裂准则研究

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。

Study on Applying of Assumption of Grain Crack with no Deformation

固体推进剂裂纹不变形假设使用条件的研究

Researches on Combustion and Processes of High Boron Content Boron-Based Fuel-Rich Solid Propellants;

高含硼富燃固体推进剂工艺和燃烧性能研究

Structural Reliability Analysis for Viscoelastic Materials of Solid Propellant;

固体推进剂类粘弹性材料结构可靠性分析

Theoretical Calculation of Ultraviolet Radiation Properties for Solid Propellant Aircraft Plume;

固体推进剂飞行器尾焰紫外辐射特性理论计算

Research on the Method to Predict the Quasi-static Mechanical Property for Solid Propellant;

固体推进剂准静态力学性能预测方法研究

The Study of Combustion Characteristics of Solid Propellants under Laser Radiation

激光辐射下固体推进剂燃烧特性及规律研究

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

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

Analysis of Mechanical Response of Composite Solid Propellants Based on ANSYS Software

基于ANSYS的复合固体推进剂力学响应分析

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