首页 | 本学科首页   官方微博 | 高级检索  
     


Interior Performances of an Impulse Thruster by Numerical Calculation
Authors:YANG Qing  WANG Li-qiong  WANG Pei-lan  HUANG Ge-de
Affiliation:1. State Key Laboratory of Explosion Science and Technology, Beijing Institute of Technology, Beijing 100081, China
2. China North Industries Corporation, Beijing 100053, China
Abstract:Impulse thruster is a kind of actuator used for trajectory correction or attitude control of some in-flight munitions and vehicles.A simple mathematical model was set up to model interior characteristics of an impulse thruster.With this model,effects of some key parameters on interior performances of the impulse thruster were studied.Results show that action time is affected significantly by nozzle throat diameter and volume of combustion chamber,while output impulse is sensitive to charge particle diameter...
Keywords:impulse thruster  trajectory correction  interior performances  numerical calculation
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《北京理工大学学报(英文版)》浏览原始摘要信息
点击此处可从《北京理工大学学报(英文版)》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号