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一种卫星软伸杆
Application NumberCN201310185036.7
董伟; 沈超; 陈涛
2013
Application Date2013-05-17
Date Available2013-09-04
Country中国
Abstract本发明涉及一种卫星软伸杆,所述卫星软伸杆包含:设置于卫星自旋轴线外围圆周上的若干子软伸杆2,用于控制各个子软伸杆2同步及等长释放的控制电机18;所述各子软伸杆进一步包含:软线缆6,用于缠绕软线缆6的缠绕轴装置12,该缠绕轴装置12进一步包含:中心转动轴29及与中心转动轴29同轴固定的线缆缠绕轴17,所述线缆缠绕轴17固定在轴向设置的缠绕轴支架7上;所述软线缆6中的一段缠绕于线缆缠绕轴7上,另一段端部设置有一端部球体19沿径向分布并穿过一球体起点保持器4;所述缠绕线轴12位于载荷舱地板26的中部,所述各个子软伸杆沿载荷舱地板26径向展开。
Language中文
Document Type专利
Identifierhttp://ir.nssc.ac.cn/handle/122/2382
Collection空间科学部
Recommended Citation
GB/T 7714
董伟,沈超,陈涛. 一种卫星软伸杆[P]. 2013-01-01.
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