管内发射两级火箭原理研究

詹高澍

弹道学报 ›› 2009, Vol. 21 ›› Issue (1) : 75-77.

弹道学报 ›› 2009, Vol. 21 ›› Issue (1) : 75-77.

管内发射两级火箭原理研究

  • 詹高澍
作者信息 +

A Study on Launching of Two step Rocket Inside the Tube

  • ZHAN Gao shu
Author information +
文章历史 +

摘要

描述了管内发射两级火箭的发射过程,将该发射过程分为4个阶段.对二级火箭的点火时间进行分析,设计并完成了二级火箭在管内与管外2种情况下开始工作的对比试验.结果表明,管内发射两级火箭的发射原理是可行的,该发射方式可提高火箭弹的速度.

Abstract

The launching process of two step rocket inside the tube was described, and the launching process was divided into four steps. Ignition time of the second solid propellant was analyzed. The contrast experiment of its starting work inside the tube and outside was designed and accomplished. The results show that launching of two step rocket working inside the tube is feasible, and the launching mode can increase the rocket velocity.

关键词

管内发射 / 火箭 / 发射试验

Key words

launching inside the tube / rocket / launching experiment

引用本文

导出引用
詹高澍. 管内发射两级火箭原理研究. 弹道学报. 2009, 21(1): 75-77
ZHAN Gao shu. A Study on Launching of Two step Rocket Inside the Tube. Journal Of Ballistics. 2009, 21(1): 75-77

参考文献

[1]詹高澍. 便携式火箭推力分解研究[D]. 南京:南京理工大学,2005.
[2]季宗德,周长省,丘光申. 火箭弹设计[M]. 北京:兵器工业出版社,1995.
[3]徐明友. 火箭外弹道学[M]. 哈尔滨:哈尔滨工业大学出版社,2004.

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