Research on Interior Ballistic of a Gas Multi-stage Cylinder Ejection

被引:1
|
作者
Huang, Mei [1 ]
Jiang, Yi
Wang, Boman [1 ]
机构
[1] Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
关键词
D O I
10.1051/matecconf/201817903005
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Aimed at increasing aircraft's leaving speed based on a determinate length of aircraft container and ensuring the aircraft's acceleration below one certain value, a new gas multi-stage cylinder ejection is proposed in this paper, and at the same time the primary design and the interior ballistic evaluating are processed. The simulation results can be used for the design of gas-catapult device and provide theoretical support for parameter optimizations in trajector.
引用
收藏
页数:6
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