[an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]Journal of Projectiles, Rockets, Missiles and Guidance >
Research on the Feasibility of Extending Rocket’s Range Using Dual-pulse Solid Rocket Motor
Received date: 2019-05-23
Online published: 2025-02-12
The range of rockets is constrained by the development of traditional solid rocket technology. In the absence of significant improvement in high-energy propellant technology, it has become increasingly difficult to further increase the range of rockets. This paper first analyzes the main factors affecting the range of rockets, and analyzes the resistance coefficient,speed and additional thrust factors of rockets with different solid rocket technology. Simulation results show that using dual-pulse rocket motor can effectively increase the range of the rocket.
Key words: dual pulse rocket motor; rocket; range; ballistic; aerodynamic force
GOU Qiuxiong , WANG Wei , YANG Xiaoying , HU Xiaoming . Research on the Feasibility of Extending Rocket’s Range Using Dual-pulse Solid Rocket Motor[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2020 , 40(3) : 79 -84 . DOI: 10.15892/j.cnki.djzdxb.2020.03.019
| [1] |
孙超, 张琳, 严聪, 等. 双脉冲固体火箭发动机概况[J]. 飞航导弹, 2013(8):72-77.
|
| [2] |
|
| [3] |
|
| [4] |
毕世龙, 陈延辉. 多脉冲发动机研究[J]. 飞航导弹, 2011(9):88-92.
|
| [5] |
张毅. 弹道导弹弹道学[M]. 长沙: 国防科技大学出版社, 1999:32-98.
|
/
| 〈 |
|
〉 |