发明名称 Deployable radiator with flexible line loop
摘要 Radiator assembly (10) for use on a spacecraft (12) is provided including at least one radiator panel assembly (26) repeatably movable between a panel stowed position (28) and a panel deployed position (36), at least two flexible lines (40) in fluid communication with the at least one radiator panel assembly (26) and repeatably movable between a stowage loop (42) and a flattened deployed loop (44).
申请公布号 US6595470(B2) 申请公布日期 2003.07.22
申请号 US20010002498 申请日期 2001.11.02
申请人 THE BOEING COMPANY 发明人 KEELER BRYAN V.;LEHTINEN ARTHUR MATHIAS;MCGEE BILLY W.
分类号 B64G1/22;B64G1/50;(IPC1-7):B64G1/46 主分类号 B64G1/22
代理机构 代理人
主权项
地址