火箭设计

微重力火箭设计中减旋方案等问题

On the Problems of Gyration Reduction etc in Microgravity Rocket Design

风切变与运载火箭设计

Wind shear and rocket design

基于整体级概念的多级固体运载火箭设计与优化

Design and optimization of multi-stage solid launch rocket based on integrated stage concept

涉及火箭设计的大部分工作已经以研制导弹为中心了。

Most of the work that has gone into the design of rockets has centered on missile development .

本课程包括实验、作业、项目设计和关于航天器和火箭设计概念的相关资料。

This course contains labs , assignments , projects , and related resources dealing with aircraft and rocketry design concepts .

传统的运载火箭设计模式是一种串行模式，即把设计结果依次展开。

The traditional design pattern of the launch vehicle is the serial mode . The design results were list in a sequence .

况且中国人的火箭设计细节，当然也不能轻易向外人泄漏，美国人不知底里，又如何指点？

Moreover , the Chinese cannot easily give out the details of their own rocket design . How can the Americans who don 't know the ins and outs of the thing give any guidance ?

表明在引射火箭设计时，应结合引射火箭的结构和流动参数对二次喷管出口面积进行优化设计，以达到最佳推力性能。

The conclusion that the optimal secondary nozzle exit area generating the maximum thrust agrees well with the numerical simulation , indicating that the exit area of secondary nozzle should be optimized according to structure and flow parameters during design .

ANSYS程序优化技术在固体火箭发动机设计中的应用

Application of ANSYS program optimization techniques to solid rocket motor design

基于CORBA的运载火箭总体设计一体化系统的实现

Implementation of Launcher Vehicle Integrated System Based on CORBA

本文的主要工作面向液体火箭发动机设计CAD技术，并选择再生冷却式液体火箭发动机推力室设计CAD技术研究作为方向。

This paper mainly focuses on CAD of LRE design , and present studies on CAD technique of recycled cooling LRE combustion chamber .

将CAD技术引入固体火箭发动机设计，可大幅提高设计效率和产品质量，缩短固体发动机研制周期，将设计者从简单的重复劳动中解放出来，有利于设计创新。

With applying technology of computer aided design to solid rocket motor design , efficiency and quality of the motor is improved , and designers are released from simple iteration to have more time on creativity .

算例分析结果表明所提出的GTO发射轨道优化设计策略的优良性能，在运载火箭总体设计中有良好的应用价值。

This approach for GTO launch trajectory optimization has been testified with predominant performance index , and has great engineering value in launch vehicle system design .

面向测控的运载火箭仿真设计与实现

Design and Realization of TT & C-Oriented Simulation of Launch Vehicle

计算机在固体火箭发动机设计与研制中的应用

Application of computers in design and development of solid rocket motors

固体火箭发动机设计是一项复杂的系统工程。

Solid rocket motor design is a complicated systems engineering .

图形变形法在固体火箭发动机设计优化中的应用

Graph Morphing applied in design optimization for solid rocket motor

工程科学中有关火箭的设计与操作的分支。

The branch of engineering science that studies rocket design and operation .

一种评估火箭结构设计的新方法

A New Method for Evaluating the Design of Rocket Structure

此项设计技术对带反向喷管的固体火箭发动机设计具有参考作用。

This technique is available for the design of SRM with reverse nozzle .

平飞固体火箭助推器设计

The booster design on flat flight solid rocket Flying

三次优化方法在火箭弹道设计中的应用

The 3-time Optimum Method Applied in Rocket Ballistic Design

一种优选探空火箭总体设计方案的方法

A Method of Optimization of Sounding Rocket Architectural Design

抑制中频不稳定性的固体火箭发动机设计

Design of Solid Propellant Rocket Engine Aiming at a Damping of the Mid-Frequency Instability

固体运载火箭弹道设计与优化

Calculation and Optimization of Solid Launch Vehicle Trajectory

运载火箭优化设计通用仿真类库设计与开发

The Design and Development of the All-purpose Simulation Class Library for Launch Vehicle Optimization Design

提出了一种对基于耗尽关机多级固体火箭概念设计的改进方法，此方法满足导弹系统主要的战技要求。

An improved method for designing a multi-stage solid rocket based depleted shutdown was provided .

旋风号火箭的设计和今后发展

Cyclone Rocket and Its Development

详细介绍了两种火箭的设计方案；并对火箭的研制进展进行了描述。

System design concepts for both of the launch vehicles are described and their development status is presented .

这艘重型运载火箭被设计用来直接将探测器送到地火转移轨道上。

The heavy lift launch vehicle is designed to directly bring the probe to the transitional Earth-Mars orbit .