[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 >
Effect of Working Time of Gas Generator on Internal Ballistic Characteristics of Cold Launch
Received date: 2024-10-15
Online published: 2025-05-15
Cold launching of rocket is a kind of launching method by means of the gas generator in the launching tube to catapult the rocket out of the launching tube, and then ignite the main engine after the projectile body leaves the tube. In order to ensure that the rocket can get enough muzzle velocity at the end of the cold launching process, a structure of the cold launcher is designed and improved, and the internal ballistic characteristics during the launching process are studied, then a two-dimensional axisymmetric model of rocket cold launcher is established. It adopts layer spread dynamic grid technology and fluid control equation to numerically simulate the internal flow field of the launcher under the same propellant quantity and different working time, and obtain the pressure inside the launcher and the motion characteristic curves of the projectile body under different working conditions. The simulation results show that under the condition of the same mass of the propellant column, the increase of the working time of the gas generator will lead to the extension of the rocket discharge time and the decrease of the discharge speed, but it will also reduce the peak pressure and acceleration in the launching tube, the rate of change in the acceleration of the rocket is more stable, and the rocket overload will be reduced during the launching process.
SUN Dongrui , ZHENG Jian , ZHANG Zhixuan . Effect of Working Time of Gas Generator on Internal Ballistic Characteristics of Cold Launch[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2025 , 45(2) : 232 -240 . DOI: 10.15892/j.cnki.djzdxb.2025.02.014
| [1] |
王成罡. 弹道导弹无依托冷发射出筒姿态动力学建模与仿真分析[D]. 哈尔滨: 哈尔滨工业大学, 2017.
|
| [2] |
赵加鹏, 张磊, 佘湖清, 等. 旁泄间隙对燃气弹射内弹道特性影响[J]. 航空动力学报, 2023, 38(10):2407-2414.
|
| [3] |
赵谢, 程洪杰, 赵媛, 等. 燃气弹射压力冲击平滑目标下的环形腔设计[J]. 固体火箭技术, 2020, 43(5):664-670.
|
| [4] |
贾轩, 杨弓熠, 段浩, 等. 燃气弹射内弹道流场数值研究[J]. 舰船科学技术, 2023, 45(10):184-189.
|
| [5] |
杨勇, 段芳芳, 王锐, 等. 一种导弹弹射用燃气发生器数值仿真设计[J]. 火工品, 2021(4):19-22.
|
| [6] |
罗叶刚, 邢玉明, 刘鑫, 等. 固-膏体燃气发生器热结构分析和仿真[J]. 北京航空航天大学学报, 2018, 44(8):1772-1779.
|
| [7] |
曾庆轩, 付文娟, 李明愉. 弹射装置的安全性设计与仿真研究[J]. 安全与环境学报, 2020, 20(4):1290-1294.
|
| [8] |
陈奇飞, 陈树伟, 刘士杰, 等. 弹射动力系统燃气发生器流热固耦合数值研究[J]. 推进技术, 2022, 43(6):203-212.
|
| [9] |
胡晓磊, 郭佳肄, 李仁凤, 等. 二次燃烧对燃气弹射内弹道影响三维数值研究[J]. 弹道学报, 2020, 32(2):67-73.
|
| [10] |
李仁凤. 燃气-蒸汽弹射流场与弹道特性研究[D]. 南京: 南京理工大学, 2017.
|
| [11] |
朱磊. 带后喷物回收喷管火箭筒发射过程不平衡冲量研究[D]. 南京: 南京理工大学, 2022.
|
| [12] |
丛龙腾. 大口径火箭弹冷发射流固耦合仿真研究[D]. 南京: 南京理工大学, 2015.
|
| [13] |
|
| [14] |
谭大成, 苗佩云. 弹射器低压室二维内弹道模型及数值研究[J]. 弹箭与制导学报, 2006, 26(4):224-226.
|
| [15] |
姜毅, 郝继光, 傅德彬. 导弹发射过程三维非定常数值模拟[J]. 兵工学报, 2008, 29(8):911-915.
|
| [16] |
曹颖, 王栋, 武晓松. 底排装置瞬态泄压过程数值模拟[J]. 四川兵工学报, 2014, 35(5):43-46.
|
| [17] |
唐垚, 姜毅, 王成德, 等. 多级活塞缸式燃气弹射内弹道的研究[J]. 固体火箭技术, 2018, 41(4):524-531.
|
| [18] |
袁永润. 航行体模型发射气炮装置研制[D]. 绵阳: 西南科技大学, 2022.
|
| [19] |
袁永润, 马国鹭, 陈万华, 等. 基于压力损失的轻气炮内弹道建模及仿真分析[J]. 火炮发射与控制学报, 2022, 43(6):15-20.
|
| [20] |
任兴鸽, 杜典, 任杰. 减后坐力燃气弹射装置的内弹道与数值分析[J]. 战术导弹技术, 2023(5):32-38.
|
| [21] |
惠卫华, 鲍福廷, 刘旸. 考虑低燃温燃气发生器试验的弹射器内弹道性能预示[J]. 固体火箭技术, 2013, 36(6):715-719.
|
| [22] |
邓春丽. 某型号发射箱箱体与燃气流固耦合分析研究[D]. 贵阳: 贵州大学, 2020.
|
/
| 〈 |
|
〉 |