发明名称 Spacecraft mast deployable thin walled hollow section comprises strips unreeled from drums by friction drive and bonded at edges
摘要 <p>A spacecraft mast deployable thin walled hollow section (3) comprises two or more carbon fibre, plastic or metal strip segment strips (2) unreeled from drums (4) by friction (6) drives (7) and joined at their edges (10) by adhesive, hook and eye or welding.</p>
申请公布号 DE10335210(A1) 申请公布日期 2005.03.10
申请号 DE2003135210 申请日期 2003.07.30
申请人 HTS - HOCH TECHNOLOGIE SYSTEME GMBH 发明人
分类号 B21C37/08;B21C37/10;B64G1/22;(IPC1-7):B21C37/00;E04H12/18 主分类号 B21C37/08
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