发明名称 Artificial satellite deployable structure having foldable/deployable element toroidal volume stored and belt attached envelope
摘要 The artificial satellite deployable structure has an envelope with a deployable element (10) and a storage means (6,7) storing the element in the folded state adjacent to the satellite. The storage is a toroid volume (5) with a belt attachment to the envelope.
申请公布号 FR2836451(A1) 申请公布日期 2003.08.29
申请号 FR20020002295 申请日期 2002.02.22
申请人 CENTRE NATIONAL D'ETUDES SPATIALES 发明人 UNAL JEAN
分类号 B64G1/22;B64G1/44;B64G1/66;H01Q15/16 主分类号 B64G1/22
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