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固体火箭助推器CAD系统软件的研究与开发

王善骏 杨余旺

计算机与现代化Issue(11):76-81,6.
计算机与现代化Issue(11):76-81,6.DOI:10.3969/j.issn.1006-2475.2014.11.017

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

王善骏 1杨余旺1

作者信息

  • 1. 南京理工大学计算机科学与工程学院,江苏 南京 210094
  • 折叠

摘要

Abstract

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

Key words

solid rocket booster/computer-aided design/interior ballistics calculation/CATIA/parametric design

分类

信息技术与安全科学

引用本文复制引用

王善骏,杨余旺..固体火箭助推器CAD系统软件的研究与开发[J].计算机与现代化,2014,(11):76-81,6.

基金项目

总装预研基金(9140A05010113xxx) (9140A05010113xxx)

江苏省科技支撑计划(BE2012386) (BE2012386)

计算机与现代化

OACSTPCD

1006-2475

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