发明名称 SPACE VEHICLE HAVING A PAYLOAD-CENTRIC CONFIGURATION
摘要 In one aspect, a space vehicle includes a structure configured to expand from a first configuration to a second configuration 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 antenna 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. In a further aspect, a space vehicle includes a payload element and at least two spacecraft-support structures attached to the periphery of the payload element. At least one of the at least two spacecraft-support structures includes a propulsion system and a tracking, telemetry and control system.
申请公布号 US2009057492(A1) 申请公布日期 2009.03.05
申请号 US20070845825 申请日期 2007.08.28
申请人 HARRIS MARK A 发明人 HARRIS MARK A.
分类号 B64G1/00;B64G1/24;B64G1/40;B64G1/52 主分类号 B64G1/00
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