| 固体火箭发动机集成方案设计系统SRMCAD |
| |
| 引用本文： | 梁国柱,张卫华,郭红杰,黄喻路,王慧玉.固体火箭发动机集成方案设计系统SRMCAD[J].固体火箭技术,2003,26(3):18-20. |
| |
| 作者姓名： | 梁国柱 张卫华 郭红杰 黄喻路 王慧玉 |
| |
| 作者单位： | 北京航空航天大学宇航学院,北京,100083 |
| |
| 摘 要： | 研制了一种固体火箭发动机集成方案设计系统软件SRMCAD。该系统采用了模块化的结构设计，共有14个模块：即系统执行控制、系统输入、系统输出、数据文件管理、热力计算、总体参数优化、指标分配、燃烧室设计、装药几何设计、内弹道计算、药柱强度校核、喷管设计、点火器设计和质量特性计算。该系统以发动机性能方案设计为主。兼顾初步的结构方案设计，能在视窗操作系统上运行。
|
| 关 键 词： | 固体推进剂火箭发动机 计算机辅助设计 系统软件 SRMCAD 集成方案设计 |
| 文章编号： | 1006-2793(2003)03-0018-03 |
| 修稿时间： | 2002年6月18日 |
Brief introduction of solid rocket motor integrated conceptual design system SRMCAD |
| |
| LIANG Guo-zhu,ZHANG Wei-hua,GUO Hong-jie,HUANG Yu-lu,WANG Hui-yu//School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing ,China..Brief introduction of solid rocket motor integrated conceptual design system SRMCAD[J].Journal of Solid Rocket Technology,2003,26(3):18-20. |
| |
| Authors: | LIANG Guo-zhu ZHANG Wei-hua GUO Hong-jie HUANG Yu-lu WANG Hui-yu//School of Astronautics Beijing University of Aeronautics and Astronautics Beijing China |
| |
| Institution: | LIANG Guo-zhu,ZHANG Wei-hua,GUO Hong-jie,HUANG Yu-lu,WANG Hui-yu//School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing 100083,China. |
| |
| Abstract: | An integrated conceptual design software system for solid rocket motors SRMCAD is developed. The system is a modular structure,has 14 modules which are system execution control, system input, system output, data file management, thermodynamic calculation, system parameter optimization, design target distribution, combustion chamber design, grain geometry design, internal ballistic calculation, grain strength verification, nozzle design, igniter design and mass property calculation. This system focuses on conceptual design of motors and preliminary structural designs. It can be run on operating system Windows on microcomputers. |
| |
| Keywords: | solid propellant rocket engine computer aided de- sign system software |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
|
