Optimizing modification on parameter of solid rocket engine

被引：0
|
作者：
Zhao, Wen-Sheng [1 ]
Tao, Shan-Zhi [1 ]
机构：
[1] 31st Res. Inst., Beijing 100074, China
来源：
| 2002年 / Journal of Propulsion Technology卷 / 23期
关键词：
Calculations - Combustors - Design - Mathematical models - Optimization - Pressure - Solid propellants;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
The difference between the actual performance and the aim of design on solid rocket engine was analyzed. The object about the parameter adjustment on project was presented. Founded the mathematics model with combustor pressure as objective function, regarded the double conditions of performance and project as restriction. Based on the calculation optimization and analysis, the design parameters of motor were adjusted.
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页码：5 / 7
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