摘要
介绍了星箭解锁系统在规定的超高真空和自身温度或温度循环及包带预紧力条件下解锁分离试验的目的、试验要求、试验技术和“风云一号”星箭解锁系统解锁分离试验的简单情况。
The paper presents the purpose,requirement、technology of the unlocking test of the unlocking and separation system of satellite and rocket under the fixed condition of the ultrahige vaccum and safe-temperature or temperation circulation and pertightening force of clamp band,and the unlocking and separation test of the unlocking system of satellite and rocket of the Satellite FY-1 is briefly described.
出处
《航天器环境工程》
1998年第3期9-17,共9页
Spacecraft Environment Engineering
关键词
星箭解锁系统
解锁分离试验
包带
超高真空
冷焊
Unlocking system of satellite and rocket
Release separation test
Belting
Ultrahigh vaccum
Cold welding
