摘要
卫星与火箭的锁紧与分离装置,是确保卫星发射成功的重要部件之一.为了提高星箭分离的可靠性,目前主要采用包带方式连接星箭对接框和包带分离技术,以提高星箭分离的可靠性.对包带的预紧力有严格要求.本文介绍了为实时监视包带预紧力而研制的系统的配置、软件和硬件设计特点以及在发射澳星过程中的应用.
The locking and departing device for satellite and launching vehicle is one of the most important units to ensure successful launch of satellite.In order to ensure the departing reliability,the wrapband is mostly adopted.Hence the preforce in the wrapband,which ensures proper connection of launching vehicle and satellite,must be strictly controlled.In this paper,the equipment,hardware, software of the system and their application in the launching task of “Aussat-B” satellite are decribed.
出处
《实验力学》
CSCD
北大核心
1993年第2期97-101,共5页
Journal of Experimental Mechanics
关键词
包带
应力测量
火箭
卫星
wrapband
stress
launching
vehicle
satellite.
