发明名称 INSTALLATION STRUCTURE OF SATELLITE EQUIPMENT OR THE LIKE IN ARTIFICIAL SATELLITE
摘要 PROBLEM TO BE SOLVED: To buffer a shock propagating on an artificial satellite structure and reaching on-satellite equipment when an unfolding mechanism such as a solar battery paddle or an antenna installed to an artificial satellite is unfolded in space. SOLUTION: Spacers 21a, 21b and inserts 12a, 12b installed in an equipment mounting panel retaining the on-satellite equipment are fastened with screws 16a, 16b, while the spacers 21a, 21b and inserts 14a, 14b embedded in a base panel 13 of the on-satellite equipment are fastened with screws 16c, 16d. Thereby, securing of rigidity and buffering of a shock are compatible.
申请公布号 JP2001122200(A) 申请公布日期 2001.05.08
申请号 JP19990300763 申请日期 1999.10.22
申请人 MITSUBISHI ELECTRIC CORP 发明人 ARIKI SHIGERU
分类号 B64G1/66;(IPC1-7):B64G1/66 主分类号 B64G1/66
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