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1. 发明申请

WO2007100447A3 SYSTEM OF STOWING AND DEPLOYING MULTIPLE PHASED ARRAYS OR COMBINATIONS OF ARRAYS AND REFLECTORS 审中-公开
标题翻译：分布和分配多个相位阵列或阵列与反射器组合的系统
公开(公告)号：WO2007100447A3
公开(公告)日：2008-01-17
申请号：PCT/US2007003012
申请日：2007-02-05
申请人： LOCKHEED CORP , HENTOSH DAVID J , EDRIDGE MICHAEL
发明人： HENTOSH DAVID J , EDRIDGE MICHAEL
IPC分类号： H04B7/185
CPC分类号： H01Q1/1228 , H01Q1/288 , H01Q3/08 , H01Q19/12 , H01Q21/062 , Y10S343/02
摘要： A spacecraft is provided that includes a spacecraft body, a phased array coupled to a side of the spacecraft body by a first deployment couple, and a reflector coupled to the side of the spacecraft body by a second deployment couple. The first and second deployment couples are configured to permit stowing the reflector and the phased array parallel to the side of the spacecraft body. The reflector and the phased array share a common launch restraint mounting point on the side of the spacecraft body. A spacecraft is also provided that includes a spacecraft body, a mounting platform coupled to a side of the spacecraft body by a deployment couple, and a plurality of phased array assemblies. Each phased array assembly has a face with elements, and is coupled to the mounting platform by a gimbal. The deployment couple and the gimbals are configured to permit stowing the phased array assemblies parallel to the side of the spacecraft body and with the face of each phased array assembly oriented in a first direction. The phased array assemblies share a common launch restraint mounting point on the side of the spacecraft body.
摘要翻译：提供了一种航天器，其包括航天器主体，通过第一部署对耦合到航天器主体的一侧的相控阵列，以及通过第二部署对耦合到航天器本体侧的反射器。第一和第二部署配对被配置为允许将反射器和相控阵列平行于航天器主体的一侧收起。反射器和相控阵在飞船身体一侧共享共同的发射限制安装点。还提供了一种航天器，其包括航天器主体，通过部署联接器联接到航天器主体的一侧的安装平台以及多个相控阵列组件。每个相控阵组件具有带有元件的面，并且通过万向节连接到安装平台。配置组件和万向架被配置为允许将相控阵组件平行于航天器主体的一侧并且每个相控阵列组件的面朝第一方向定向。相控阵组件在飞船身体侧面共享一个共同的发射限制安装点。

2. 发明申请

WO2007109380A3 SATELLITE WITH DEPLOYABLE, ARTICULATABLE THERMAL RADIATORS 审中-公开
标题翻译：卫星与可配置的热电偶散热器
公开(公告)号：WO2007109380A3
公开(公告)日：2008-10-02
申请号：PCT/US2007060501
申请日：2007-01-12
申请人： LOCKHEED CORP , MCKINNON DOUGLAS V , BROWN DAVID M , HENTOSH DAVID J
发明人： MCKINNON DOUGLAS V , BROWN DAVID M , HENTOSH DAVID J
IPC分类号： B64G1/22 , B64G1/52
CPC分类号： B64G1/222 , B64G1/503
摘要： A satellite (50) is disclosed having at least one deployable thermal radiator (64). Once deployed, this thermal radiator (64) may be repositioned. In one embodiment, the deployed thermal radiator (64) may be moved about a first axis (74), about a second axis (76), or both to move the deployed thermal radiator (64) from one deployed position to another deployed position.
摘要翻译：公开了一种具有至少一个可展开散热器（64）的卫星（50）。一旦部署，该热散热器（64）可以重新定位。在一个实施例中，部署的热辐射器（64）可围绕第一轴线（74）绕第二轴线（76）或两者移动，以将部署的散热器（64）从一个展开位置移动到另一展开位置。

3. 发明申请

WO2014126591A3 DEPLOYABLE RADIATOR HAVING AN INCREASED VIEW FACTOR 审中-公开
标题翻译：具有增加视角因子的可分散式散热器
公开(公告)号：WO2014126591A3
公开(公告)日：2015-06-18
申请号：PCT/US2013027349
申请日：2013-02-22
申请人： LOCKHEED CORP
发明人： GOODZEIT NEIL E , WONG HAMILTON , HENTOSH DAVID J
IPC分类号： B64G1/50
CPC分类号： B64G1/503 , B64G1/506
摘要： A geostationary earth orbit (GEO) spacecraft is disclosed that includes a body with north, east, south, and west sides and a north-south axis. The spacecraft has at least one deployable radiator rotatably coupled to the body. The deployable radiator has a stowed position proximate to one of the east and west sides and a deployed position that is greater than 90 degrees from the north south axis in a direction away from the respective one of the east and west sides.
摘要翻译：披露了一个地球静止轨道（GEO）航天器，其中包括一个具有北，东，南，西三面和南北轴的物体。航天器具有可旋转地联接到主体的至少一个可展开的辐射体。可部署的散热器具有靠近东西两侧的收起位置，并且在远离东西两侧的方向上从北南轴线大于90度的展开位置。

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