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轻型动能拦截器固体控制发动机方案分析
引用本文:李世鹏,张平.轻型动能拦截器固体控制发动机方案分析[J].推进技术,1999,20(2):99-102.
作者姓名:李世鹏  张平
作者单位:北京理工大学机电工程学院,北京,100081
摘    要:对国外轻型动能杀伤飞行器(KKV)采用固体燃气发生器作动力的控制发动机方案进行了分析,比较了变流率燃气发生器、装药设计和脉宽调制变推力执行机构方案等,提出了适合国内技术条件的可行方案,并讨论了有关技术问题。

关 键 词:动能拦截器  燃气发生器  姿控火箭发动机  方案

ANALYSIS OF SOLID PROPELLANT CONTROL THRUSTER SCHEMES FOR SMALL KKV
Li Shipeng and Zhang Ping.ANALYSIS OF SOLID PROPELLANT CONTROL THRUSTER SCHEMES FOR SMALL KKV[J].Journal of Propulsion Technology,1999,20(2):99-102.
Authors:Li Shipeng and Zhang Ping
Institution:School of Electro Mechanical Engineering,Beijing Inst.of Technology,Beijing,100081;School of Electro Mechanical Engineering,Beijing Inst.of Technology,Beijing,100081
Abstract:The schemes of kinetic kill vehicles(KKV)that use solid propellant gas generator as power provider are reviewed.The solid propellant gas generator with variable flow rate,the grain design and the thrusters with variable thrust by PWM technique are discussed,and a feasible practical scheme suitable for domestic study is presented.
Keywords:inetic energy    weapon  Gas generator  Attitude control rocket engine  Proposal research  
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