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 US7686255(B2) 申请公布日期 2010.03.30
申请号 US20070845825 申请日期 2007.08.28
申请人 RAYTHEON COMPANY 发明人 HARRIS MARK A.
分类号 B64G1/10 主分类号 B64G1/10
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