首页 | 本学科首页   官方微博 | 高级检索  
     检索      

轨姿控发动机动态推力与推力矢量测试系统研制
引用本文:耿卫国,朱子环.轨姿控发动机动态推力与推力矢量测试系统研制[J].宇航计测技术,2015,35(6):28.
作者姓名:耿卫国  朱子环
作者单位:1、北京航天试验技术研究所, 北京 100074
摘    要:针对目前轨姿控发动机动态推力与推力矢量测试系统测量精度低、测试覆盖面不全及操作的复杂性,研制了一套基于压电测力平台的动态推力与推力矢量测试系统。此系统的研制攻克了测力平台结构参数优化技术、标准信号发生器设计技术、测试相间干扰处理技术等五项关键技术点.实现了连续脉冲力及多方向力的测量,系统操作可靠、便捷,各项测试指标满足总体要求,为动态推力及推力矢量测试提供了手段。

关 键 词:轨姿控发动机  动态推力  推力矢量  

Development of Dynamic Thrust and Thrust Vector Measurement System for Orbit and Attitude Engine
GENG Wei-guo,ZHU Zi-huan.Development of Dynamic Thrust and Thrust Vector Measurement System for Orbit and Attitude Engine[J].Journal of Astronautic Metrology and Measurement,2015,35(6):28.
Authors:GENG Wei-guo  ZHU Zi-huan
Institution:1、Beijing Institute of Aerospace testing Technology,Beijing 100074
Abstract:Aiming at the problems of the low measurement accuracy, incomplete test coverage and complex operation of the dynamic thrust and thrust vector measurement system for orbit and attitude engine at present, the track dynamic thrust and thrust vector measurement system based on the piezoelectric force measurement platform is developed.The optimization design technology of structure parameters of the measurement force, the standard signal generator design technology, the interphase interference processing technology and so on five key technical points have been overcome.The measurement of the continuous pulse force and multi direction force has been realized , the system operation is reliable and convenient, the general requirement is met for the test targets ,the means of dynamic thrust and thrust vector test is provided .
Keywords:Orbit and Attitude Engine  Dynamic thrust  Thrust vector  
本文献已被 CNKI 等数据库收录!
点击此处可从《宇航计测技术》浏览原始摘要信息
点击此处可从《宇航计测技术》下载免费的PDF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