发明名称 Earth orbiting, sun following satellite
摘要 The includes a reduced number of solar panels with various sides used for different purposes. Satellite sides are available for various instruments, such as aerials, drive units, adaptors etc.. The free sides without solar cells can be used for waste heat radiation.The satellite comprises simple accommodation of foldable solar panels without complex aligning and follower mechanisms. It uses a gravity gradient stabilisation for the yaw and pitch axes. The panel aligning is carried out by magnetic coils.
申请公布号 DE4440658(A1) 申请公布日期 1996.05.15
申请号 DE19944440658 申请日期 1994.11.14
申请人 OHB OPTO-ELEKTRONIK UND -HYDRAULIK-SYSTEM GMBH, 28359 BREMEN, DE 发明人 GINATI, AMNON, DIPL.-ING., 28359 BREMEN, DE
分类号 B64G1/10;B64G1/24;B64G1/28;B64G1/32;B64G1/34;B64G1/44;B64G1/50;(IPC1-7):B64G1/10;H01L31/052 主分类号 B64G1/10
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