固体火箭助推器CAD系统软件的研究与开发  

Research and Implementation of Solid Rocket Boosters CAD System Software

作　　者：王善骏 杨余旺[1] 

机构地区：[1]南京理工大学计算机科学与工程学院,江苏南京210094

出　　处：《计算机与现代化》2014年第11期76-81,共6页Computer and Modernization

基　　金：总装预研基金(9140A05010113xxx);江苏省科技支撑计划(BE2012386)

摘　　要：针对固体火箭助推器的设计问题,本文将CAD技术运用于火箭研制过程,结合无人机助推发射系统设计与仿真软件,探讨当前固体火箭助推器CAD系统发展现状与特点,研究固体火箭助推器CAD系统的组成与实现方案,开发一套固体火箭助推器设计与仿真系统软件。系统集成助推器结构设计、参数化绘图、数据库管理3个模块。系统具有友好的操作界面,推进剂模块与装药设计模块之间进行了关联,可有效完成助推器产品管理,只需输入少量数据,便可快速构造助推器,为助推器方案论证提供了有力工具。For the problem of the solid rocket booster design, this article takes rocket CAD technology used in the development process, combined with the UAV launch assist system design and simulation software, explores current solid rocket boosters CAD system development status and characteristics, studies the composition and implementation of solid rocket booster CAD system, develops a solid rocket booster system design and simulation software. Booster system integrates design, parametric drawing, da-tabase management three modules. The system has a friendly user interface, makes the association between the propellant charge module and design module, which can effectively complete the booster product management, simply enter a small amount of data, you can quickly construct booster. It provides a powerful tool for booster program demonstration.

关 键 词：固体火箭助推器 计算机辅助设计 内弹道计算 CATIA 参数化设计 

分 类 号：TP391.9[自动化与计算机技术—计算机应用技术]