发明名称 A SPACE VEHICLE HAVING A PAYLOAD-CENTRIC CONFIGURATION
摘要 <p>In one aspect, a space vehicle includes a structure configured to expand from a first configuration to a second con-figuration and at least two equipment compartments attached to the periphery of the structure. The structure includes at least one of an antenna mesh, a light-shielding mesh, an optical reflector mesh and a net. In another aspect, a space vehicle includes an an-tenna structure configured to expand from a first configuration to a second configuration and at least two equipment compartments attached to the periphery of the antenna structure. At least one of the at least two equipment components include a solar panel, a propulsion system and an antenna feed.</p>
申请公布号 CA2694328(C) 申请公布日期 2015.07.21
申请号 CA20082694328 申请日期 2008.08.04
申请人 RAYTHEON COMPANY 发明人 HARRIS, MARK A.
分类号 B64G1/00;B64G1/22;B64G1/24;B64G1/36;B64G1/40;B64G1/52;B64G1/66 主分类号 B64G1/00
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