| 火箭发动机储能点火的分析与设计 |
| |
| 引用本文： | 李建飞,郑海龙,魏峰,刘春平. 火箭发动机储能点火的分析与设计[J]. 电子测试, 2013, 0(11): 17-20,16 |
| |
| 作者姓名： | 李建飞 郑海龙 魏峰 刘春平 |
| |
| 作者单位： | 中国航天科工集团六院41所,呼和浩特010010 |
| |
| 摘 要： | 为了实现导弹上的多个小的火箭发动机同时点火,每个小发动机的点火电路中可以配置储能元件,利用储能电容和电感振荡放电产生的电流对小发动机进行点火工作,从而降低对弹上一次电源功率的要求。利用设计的储能电路和3个电点火管,进行了储能点火试验,验证了该储能点火的可行性。
|
| 关 键 词： | 火箭发动机 储能点火 储能电路 |
Analysis and Design of reserve energy ignition in Rocket Motor |
| |
| Li Jianfei,Zheng Hailong,The,st Institute of the Sixth Academy of China Mongolia Hohhot Wei Feng,Liu Chunping. Analysis and Design of reserve energy ignition in Rocket Motor[J]. Electronic Test, 2013, 0(11): 17-20,16 |
| |
| Authors: | Li Jianfei Zheng Hailong The st Institute of the Sixth Academy of China Mongolia Hohhot Wei Feng Liu Chunping |
| |
| Affiliation: | Aerospace Science ＆ Industry Corporation, Inner 010010, China) |
| |
| Abstract: | In order that many small Rocket Motor in the missile ignite simultaneously, every ignition circuit of small Motor can config reserve energy element, it uses the current that is produced by oscillation discharging of reserve energy capacity and inductance to ignite small Motor, so it can reduce the power of the power supply that is on the missile. Making ues of reserve energy circuit designed and three igniter tubes, experiment have been finished, it testified feasibility of the reserve energy ignition. |
| |
| Keywords: | Rocket Motor reserve energy ignition reserve energy circuit |
| 本文献已被 维普 等数据库收录！ |
|
