节点文献
固体火箭发动机性能预示
Performance Prediction of Solid Propellant Rocket Motors
【摘要】 编制了固体火箭发动机性能预示软件 ,以美国的 AIM发动机和法国的 SEP发动机为例进行了比冲预示 ,并与美、英、法、德、意等国软件的预示结果进行了比较。计算表明 ,该软件达到了国外同等水平的预示精度 ,可用于导弹总体设计、发动机优化设计
【Abstract】 A software of performance prediction for solid rocket motors was developed,and predicted results of the performances for AIM motor (Naval Weapons Center,USA) and SEP motor(France) as samples with present software are presented.Compared with that of USA,France,Germany,United Kingdom and Italy softwares ,the prediction precision of present software is agreed with that of the above mentioned foreign softwares,and it can be used in the design of missile system and solid rocket motor optimization.
【关键词】 固体推进剂火箭发动机;
比冲;
性能预测;
【Key words】 solid propellant rocket motor; specific impulse; performance prediction;
【Key words】 solid propellant rocket motor; specific impulse; performance prediction;
【基金】 国防科技重点实验室试点基金项目!( No:96JS60 .6.1 .KG0 1 0 5)
- 【文献出处】 固体火箭技术 ,JOURNAL OF SOLID ROCKET TECHNOLOGY , 编辑部邮箱 ,2000年01期
- 【分类号】V435
- 【被引频次】9
- 【下载频次】241