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加速度对固体火箭发动机内弹道性能的影响
引用本文:张如洲,张平,李葆江,魏英华,张钢锤,郭彤,南宝江,王杰,马喜梅.加速度对固体火箭发动机内弹道性能的影响[J].推进技术,2000,21(3):6-8.
作者姓名:张如洲  张平  李葆江  魏英华  张钢锤  郭彤  南宝江  王杰  马喜梅
作者单位:1. 北京理工大学,机电工程学院,北京,100081
2. 陕西动力机械研究所,陕西,西安,710025
基金项目:国家重点实验室基金项目
摘    要:用片型装药火箭发动机和含铝复合推进剂,研究了加速度对固体火箭发动机内弹道性能的影响。研究结果表明,在加速度70g的条件下,2010推进剂的平均效应燃速比r^-a/r^0高达1.515,固体火箭发动机的内弹道性能呈现明显的变化。该项研究对发动机设计有实际意义。

关 键 词:固体推进剂火箭发动机  内弹道性能  燃速

Acceleration effects on internal ballistics performance of solid rocket motor
ZHANG Ruzhou,ZHANG Ping,Li Baojiang,Wei Yinghu,Zhang Gangchui,Guo Tong,Nan Baojiang,Wang Jie and Ma Ximei.Acceleration effects on internal ballistics performance of solid rocket motor[J].Journal of Propulsion Technology,2000,21(3):6-8.
Authors:ZHANG Ruzhou  ZHANG Ping  Li Baojiang  Wei Yinghu  Zhang Gangchui  Guo Tong  Nan Baojiang  Wang Jie and Ma Ximei
Institution:School of Electron Mechanical Engineering,Beijing Inst of Technology, Beijing 100081,China;School of Electron Mechanical Engineering,Beijing Inst of Technology, Beijing 100081,China;School of Electron Mechanical Engineering,Beijing Inst of Technology, Beijing 100081,China;School of Electron Mechanical Engineering,Beijing Inst of Technology, Beijing 100081,China;Shaanxi Inst;Shaanxi Inst;Shaanxi Inst;Shaanxi Inst;Shaanxi Inst
Abstract:The experimental study of the acceleration effects on the interna ballistics performance of solid rocket motor was presented Combustion test was conducted at the AET 3 type high acceleration test stand The aluminized composite solid propellant were tested in unidirectional burning propellant slab motor The experimental results indicate that the average burning rate augmentation ratio a / r 0 of propellant 2010 is as high as 1 515 at 70 g ,the internal ballistics performance of solid rocket motor exhibits a significant change It is useful for design of solid rocket motor
Keywords:Solid propellant rocket engine  Acceleration  Aluminized propellant  Interior ballistic performance  Burning rate
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