摘要
卫星火箭发动机推力矢量测试,是一项高新技术火箭测试技术。根据某卫星液体火箭发动机推力矢量的特点和测量要求,阐述了待测推力矢量参数的定义,然后对转台测试原理和计算方法进行了简单的介绍。
The thrust vector test of liquid rocket engine on satellite is a high and new technology. Based on the characteristics and measuring requirements of the thrust vector of the liquid rocket engine, the thrust parameter definition is elaborated and then the rotating table test principle and calculation method is introduced in this paper.
出处
《机械管理开发》
2008年第1期25-26,共2页
Mechanical Management and Development
关键词
液体火箭发动机
推力偏心
转台
Liquid rocket engine
Thrust misalignment
Rotating Table
