发明名称 ELECTRIC ENERGIZING PATH SYSTEM FOR SOLAR LIGHT GENERATOR OF SATELLITE MISSILE
摘要 The invention relates to an electrical current conductor track system for flexible, foldable or reelable space vehicle solar generators. The solar generators are composed of a plurality of modular carrier foil sections (SPA1-7). In order to construct such a current conductor track system in such a way that it meets the high requirements imposed in space, it is proposed that the current conductor tracks (10) are constructed in integrated form as an extremely thin layer on copper-clad carrier foil sections using the photoresist etching method. In addition, the current conductor tracks (10) should be constructed at section conductor track junctions (14) of the carrier foil sections in the fashion of a piano (butt) hinge, the projecting ends in each case meeting the welding zones of the next carrier foil section and being welded thereto. <IMAGE>
申请公布号 JPS58196065(A) 申请公布日期 1983.11.15
申请号 JP19830044521 申请日期 1983.03.18
申请人 MESSERSCHMITT BOLKOW BLOHM GMBH 发明人 UORUFUGANKU RERUSHIYU
分类号 B64G1/44;H01L31/02;H01L31/042;H01L31/05;H02S30/20 主分类号 B64G1/44
代理机构 代理人
主权项
地址