摘要
为满足长寿命大型卫星控制系统的需要 ,设计和研制了一种长寿命、大动量矩的动量飞轮。在介绍了国外大动量矩的动量飞轮产品的基础上 ,论述了 5 5N·m·s飞轮的设计技术和关键技术。给出了样机的测试结果并与国外同类产品的性能进行了比较。结果表明 ,样机的设计原理正确。
To meet the requirements of the high accuracy, long life large scale satellite, the long life and big momentum wheel must be designed and developed. This article mainly introduces the general situation of the big momentum flywheel in other countries as well as the design technique of 55N·m·s wheel.
出处
《上海航天》
2002年第1期8-12,16,共6页
Aerospace Shanghai
