发明名称 Satellite with enhanced thermal rejection
摘要 <p>The satellite has at least one face (5) acting as a thermal radiator for on-board instruments and positioned in the solar radiation trajectory. It also has a solar generating panel (7) which constantly faces towards the sun and projects from the radiator face (5), and a screen (14) which is joined to the solar panel and interrupts the solar radiation moving towards the face (5). The solar panel is mounted in the centre of the radiator face, and the screen (14) is connected to it by an arm (15) joined to the panel's supporting leg (10). The radiator face can be on the north- or south-facing surface of the satellite platform, and it has a coating with a high infrared emission level.</p>
申请公布号 EP0887260(A1) 申请公布日期 1998.12.30
申请号 EP19980401320 申请日期 1998.06.03
申请人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE 发明人 BARD, MAX
分类号 B64G1/44;B64G1/50;(IPC1-7):B64G1/50 主分类号 B64G1/44
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