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公开(公告)号：US10749959B2
公开(公告)日：2020-08-18
申请号：US16245504
申请日：2019-01-11
申请人： Vector Launch Inc.
摘要： Systems, methods, and software described herein provide enhancements for managing data storage in a spaceborne or airborne platform. In one implementation, an airborne device in an airborne platform may identify a request to store a data object in a storage pool provided by a plurality of airborne devices. The airborne device will further identify at least one airborne device for storing the data object from the plurality of airborne devices, and communicate the data object to the at least one airborne device.
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公开(公告)号：US10538348B2
公开(公告)日：2020-01-21
申请号：US15383968
申请日：2016-12-19
申请人： Vector Launch Inc.
发明人： Brian James Riskas
摘要： Provided herein are various improvements to satellite or payload deployment systems and equipment. In one example, a satellite deployment apparatus is provided. The satellite deployment apparatus includes opposing retention members configured to engage protrusions of a satellite and hold the satellite with respect to a baseplate. The satellite deployment apparatus includes at least one pusher element configured to preload a deployment force on the satellite against the opposing retention members when the protrusions of the satellite are captive in the opposing retention members, and a deployment mechanism configured to spread the opposing retention members responsive to triggering by an actuator system and release the protrusions of the satellite for deployment of the satellite away from the baseplate using at least the deployment force.
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公开(公告)号：US20200010220A1
公开(公告)日：2020-01-09
申请号：US16028797
申请日：2018-07-06
申请人： Vector Launch, Inc.
发明人： Raymond Edward Fraze
摘要： A self-mating modular satellite bus includes a plurality of side panels each having a front surface flanked by a first longitudinal edge and a second longitudinal edge, wherein the first longitudinal edge of each side panel is nested with the second longitudinal edge of an adjacent side panel. The longitudinal edges, when superimposed, form a joggle. A method of producing the modular satellite bus includes forming a plurality of the panels, aligning the first longitudinal edge of each side panel with the second longitudinal edge of an adjacent side panel, such that the first longitudinal edge of each side panel is nested with the second longitudinal edge of the adjacent side panel, and securing the first longitudinal edge of each side panel to the second longitudinal edge of the adjacent side panel.
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公开(公告)号：US20190280764A1
公开(公告)日：2019-09-12
申请号：US16422516
申请日：2019-05-24
申请人： Vector Launch Inc.
发明人： Shaun Coleman , Darren D. Garber
摘要： Systems, methods, and software described herein provide enhancements for deploying software payloads in satellite systems. In one example, a satellite device comprises a communication interface configured to receive software payloads for execution, and an execution system configured to execute ones of the software payloads as associated virtual nodes that share resources of the satellite device to at least perform activities using one or more on-board systems of the satellite device. The execution system is configured to transfer state information related to execution of ones of the virtual nodes to at least another device over the communication interface, wherein the state information comprises data related to the activities.
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公开(公告)号：US20190253134A1
公开(公告)日：2019-08-15
申请号：US15892854
申请日：2018-02-09
申请人： Vector Launch Inc.
发明人： Shaun Coleman , John Metzger , Darren D. Garber
CPC分类号： H04B7/18519 , H04B7/18513 , H04B7/18521 , H04B7/18597 , H04W72/085
摘要： Various enhanced operations and orbital techniques for satellite devices are discussed herein. In one example, a method of operating an orbital satellite platform is provided. The method includes establishing relative distances between a plurality of satellite devices, and performing temporary adjustments to the relative distances between the satellite devices. The method also includes directing at least communication processes among the satellite devices based at least in part on the temporary adjustments to the relative distances.
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公开(公告)号：US20190165852A1
公开(公告)日：2019-05-30
申请号：US16245420
申请日：2019-01-11
申请人： Vector Launch Inc.
发明人： Shaun B. Coleman , Darren D. Garber
摘要： Systems, methods, and software described herein provide enhancements for deploying applications in spaceborne and airborne systems, among others. In one example, an airborne or spaceborne physical node comprises a communication interface configured to receive software payloads, and logistical control elements of the physical node. The physical node further comprises a virtualized execution system configured to execute ones of the software payloads deployed on the physical node as associated virtual nodes that share resources of the physical node.
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公开(公告)号：US10305582B2
公开(公告)日：2019-05-28
申请号：US16137862
申请日：2018-09-21
申请人： Vector Launch Inc.
发明人： Shaun Coleman , Darren D. Garber
摘要： Systems, methods, and software described herein provide enhancements for deploying applications in satellite systems. In one example, a satellite system comprises a communication interface configured to receive software payloads, and logistical control elements of the satellite system. The satellite system further comprises a virtualized execution system configured to execute ones of the software payloads deployed on the satellite system as associated virtual nodes that share resources of the satellite system.
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公开(公告)号：US20180170586A1
公开(公告)日：2018-06-21
申请号：US15383968
申请日：2016-12-19
申请人： Vector Launch Inc.
发明人： Brian James Riskas
摘要： Provided herein are various improvements to satellite or payload deployment systems and equipment. In one example, a satellite deployment apparatus is provided. The satellite deployment apparatus includes opposing retention members configured to engage protrusions of a satellite and hold the satellite with respect to a baseplate. The satellite deployment apparatus includes at least one pusher element configured to preload a deployment force on the satellite against the opposing retention members when the protrusions of the satellite are captive in the opposing retention members, and a deployment mechanism configured to spread the opposing retention members responsive to triggering by an actuator system and release the protrusions of the satellite for deployment of the satellite away from the baseplate using at least the deployment force.
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公开(公告)号：US09991951B2
公开(公告)日：2018-06-05
申请号：US15626929
申请日：2017-06-19
申请人： Vector Launch Inc.
发明人： Shaun Coleman , Darren D. Garber
CPC分类号： H04B7/18519 , G06F9/45533 , G06F2009/4557 , G06K9/0063 , G06K9/00677 , G06K9/00979 , H04B7/18521 , H04L67/1068 , H04L67/125 , H04L67/34
摘要： Systems, methods, and software described herein provide enhancements for deploying applications in satellites. In one example, a satellite device includes a communication interface and a virtualized execution system. The virtualized execution system is configured to receive state information via the communication interface from at least a peer satellite device related to execution of one or more software payloads by the peer satellite device, and execute one or more virtual nodes based at least on the state information.
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公开(公告)号：US20180123681A1
公开(公告)日：2018-05-03
申请号：US15859978
申请日：2018-01-02
申请人： Vector Launch Inc.
发明人： Shaun Coleman , Darren D. Garber
CPC分类号： H04B7/18519 , G06F9/45558 , G06F2009/45579 , G06F2009/45583 , H04B7/18521 , H04L41/0668 , H04L67/10 , H04L67/1078 , H04L67/125 , H04L67/34
摘要： Systems, methods, and software described herein provide enhancements for deploying applications in satellite systems. In one example, a satellite system comprises a communication interface configured to receive software payloads, and a satellite control system configured to operate logistical control elements of the satellite system. The satellite system further comprises a virtualized execution system configured to execute ones of the software payloads deployed on the satellite system as associated virtual nodes that share resources of the satellite system.
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