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公开(公告)号：US11840498B2
公开(公告)日：2023-12-12
申请号：US16953450
申请日：2020-11-20
申请人： Skeyeon, Inc.
IPC分类号： C07C259/06 , H04B7/185 , G01S19/39 , B64G1/42 , B64G1/10 , H04B7/195 , B64G1/44 , A61P35/00 , G01S13/90 , B64G1/66
CPC分类号： C07C259/06 , A61P35/00 , B64G1/1021 , B64G1/425 , B64G1/443 , G01S19/39 , H04B7/18513 , H04B7/195 , B64G1/1028 , B64G1/1035 , B64G1/66 , G01S13/90
摘要： A satellite system operates at altitudes between 180 km and 350 km relying on vehicles including an engine to counteract atmospheric drag to maintain near-constant orbit dynamics. The system operates at altitudes that are substantially lower than traditional satellites, reducing size, weight and cost of the vehicles and their constituent subsystems such as optical imagers, radars, and radio links. The system can include a large number of lower cost, mass, and altitude vehicles, enabling revisit times substantially shorter than previous satellite systems. The vehicles spend their orbit at low altitude, high atmospheric density conditions that have heretofore been virtually impossible to consider for stable orbits. Short revisit times at low altitudes enable near-real time imaging at high resolution and low cost. At such altitudes, the system has no impact on space junk issues of traditional LEO orbits, and is self-cleaning in that space junk or disabled craft will de-orbit.
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公开(公告)号：US10858309B2
公开(公告)日：2020-12-08
申请号：US16129210
申请日：2018-09-12
申请人： Skeyeon, Inc.
IPC分类号： B64D1/10 , C07C259/06 , H04B7/185 , G01S19/39 , B64G1/42 , B64G1/10 , H04B7/195 , B64G1/44 , A61P35/00 , G01S13/90 , B64G1/66
摘要： A satellite system operates at altitudes between 180 km and 350 km relying on vehicles including an engine to counteract atmospheric drag to maintain near-constant orbit dynamics. The system operates at altitudes that are substantially lower than traditional satellites, reducing size, weight and cost of the vehicles and their constituent subsystems such as optical imagers, radars, and radio links. The system can include a large number of lower cost, mass, and altitude vehicles, enabling revisit times substantially shorter than previous satellite systems. The vehicles spend their orbit at low altitude, high atmospheric density conditions that have heretofore been virtually impossible to consider for stable orbits. Short revisit times at low altitudes enable near-real time imaging at high resolution and low cost. At such altitudes, the system has no impact on space junk issues of traditional LEO orbits, and is self-cleaning in that space junk or disabled craft will de-orbit.
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公开(公告)号：US20210078942A1
公开(公告)日：2021-03-18
申请号：US16953450
申请日：2020-11-20
申请人： Skeyeon, Inc.
摘要： A satellite system operates at altitudes between 180 km and 350 km relying on vehicles including an engine to counteract atmospheric drag to maintain near-constant orbit dynamics. The system operates at altitudes that are substantially lower than traditional satellites, reducing size, weight and cost of the vehicles and their constituent subsystems such as optical imagers, radars, and radio links. The system can include a large number of lower cost, mass, and altitude vehicles, enabling revisit times substantially shorter than previous satellite systems. The vehicles spend their orbit at low altitude, high atmospheric density conditions that have heretofore been virtually impossible to consider for stable orbits. Short revisit times at low altitudes enable near-real time imaging at high resolution and low cost. At such altitudes, the system has no impact on space junk issues of traditional LEO orbits, and is self-cleaning in that space junk or disabled craft will de-orbit.
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公开(公告)号：US10715245B2
公开(公告)日：2020-07-14
申请号：US15868812
申请日：2018-01-11
申请人： Skeyeon, Inc.
发明人： Dan Nobbe , Ronald E. Reedy
摘要： A satellite system operates at altitudes between 100 and 350 km relying on vehicles including a self-sustaining ion engine to counteract atmospheric drag to maintain near-constant orbit dynamics. The system operates at altitudes that are substantially lower than traditional satellites, reducing size, weight and cost of the vehicles and their constituent subsystems such as optical imagers, radars, and radio links. The system can include a large number of lower cost, mass, and altitude vehicles, enabling revisit times substantially shorter than previous satellite systems. The vehicles spend their orbit at low altitude, high atmospheric density conditions that have heretofore been virtually impossible to consider for stable orbits. Short revisit times at low altitudes enable near-real time imaging at high resolution and low cost. At such altitudes, the system has no impact on space junk issues of traditional LEO orbits, and is self-cleaning in that space junk or disabled craft will de-orbit.
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公开(公告)号：US20240317677A1
公开(公告)日：2024-09-26
申请号：US18519989
申请日：2023-11-27
申请人： Skeyeon, Inc.
IPC分类号： C07C259/06 , A61P35/00 , B64G1/10 , B64G1/42 , B64G1/44 , B64G1/66 , G01S13/90 , G01S19/39 , H04B7/185 , H04B7/195
CPC分类号： C07C259/06 , A61P35/00 , B64G1/1021 , B64G1/425 , B64G1/443 , G01S19/39 , H04B7/18513 , H04B7/195 , B64G1/1028 , B64G1/1035 , B64G1/66 , G01S13/90
摘要： A satellite system operates at altitudes between 180 km and 350 km relying on vehicles including an engine to counteract atmospheric drag to maintain near-constant orbit dynamics. The system operates at altitudes that are substantially lower than traditional satellites, reducing size, weight and cost of the vehicles and their constituent subsystems such as optical imagers, radars, and radio links. The system can include a large number of lower cost, mass, and altitude vehicles, enabling revisit times substantially shorter than previous satellite systems. The vehicles spend their orbit at low altitude, high atmospheric density conditions that have heretofore been virtually impossible to consider for stable orbits. Short revisit times at low altitudes enable near-real time imaging at high resolution and low cost. At such altitudes, the system has no impact on space junk issues of traditional LEO orbits, and is self-cleaning in that space junk or disabled craft will de-orbit.
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6.发明申请公开(公告)号：US20200343966A1
公开(公告)日：2020-10-29
申请号：US16925081
申请日：2020-07-09
申请人： Skeyeon, Inc.
发明人： Dan Nobbe , Ronald E. Reedy
摘要： A satellite system operates at altitudes between 100 and 350 km relying on vehicles including a self-sustaining ion engine to counteract atmospheric drag to maintain near-constant orbit dynamics. The system operates at altitudes that are substantially lower than traditional satellites, reducing size, weight and cost of the vehicles and their constituent subsystems such as optical imagers, radars, and radio links. The system can include a large number of lower cost, mass, and altitude vehicles, enabling revisit times substantially shorter than previous satellite systems. The vehicles spend their orbit at low altitude, high atmospheric density conditions that have heretofore been virtually impossible to consider for stable orbits. Short revisit times at low altitudes enable near-real time imaging at high resolution and low cost. At such altitudes, the system has no impact on space junk issues of traditional LEO orbits, and is self-cleaning in that space junk or disabled craft will de-orbit.
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公开(公告)号：US10590068B2
公开(公告)日：2020-03-17
申请号：US15868794
申请日：2018-01-11
申请人： Skeyeon, Inc.
IPC分类号： B64G1/10 , C07C259/06 , H04B7/185 , G01S19/39 , B64G1/42 , H04B7/195 , B64G1/44 , A61P35/00 , G01S13/90 , B64G1/66
摘要： A satellite system operates at altitudes between 180 km and 350 km relying on vehicles including an engine to counteract atmospheric drag to maintain near-constant orbit dynamics. The system operates at altitudes that are substantially lower than traditional satellites, reducing size, weight and cost of the vehicles and their constituent subsystems such as optical imagers, radars, and radio links. The system can include a large number of lower cost, mass, and altitude vehicles, enabling revisit times substantially shorter than previous satellite systems. The vehicles spend their orbit at low altitude, high atmospheric density conditions that have heretofore been virtually impossible to consider for stable orbits. Short revisit times at low altitudes enable near-real time imaging at high resolution and low cost. At such altitudes, the system has no impact on space junk issues of traditional LEO orbits, and is self-cleaning in that space junk or disabled craft will de-orbit.
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公开(公告)号：US20190016672A1
公开(公告)日：2019-01-17
申请号：US16129210
申请日：2018-09-12
申请人： Skeyeon, Inc.
IPC分类号： C07C259/06 , A61P35/00
摘要： A satellite system operates at altitudes between 180 km and 350 km relying on vehicles including an engine to counteract atmospheric drag to maintain near-constant orbit dynamics. The system operates at altitudes that are substantially lower than traditional satellites, reducing size, weight and cost of the vehicles and their constituent subsystems such as optical imagers, radars, and radio links. The system can include a large number of lower cost, mass, and altitude vehicles, enabling revisit times substantially shorter than previous satellite systems. The vehicles spend their orbit at low altitude, high atmospheric density conditions that have heretofore been virtually impossible to consider for stable orbits. Short revisit times at low altitudes enable near-real time imaging at high resolution and low cost. At such altitudes, the system has no impact on space junk issues of traditional LEO orbits, and is self-cleaning in that space junk or disabled craft will de-orbit.
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9.发明公开公开(公告)号：US20230327749A1
公开(公告)日：2023-10-12
申请号：US18205611
申请日：2023-06-05
申请人： Skeyeon, Inc.
发明人： Dan Nobbe , Ronald E. Reedy
CPC分类号： H04B7/18513 , H04B7/18534 , H04W84/06 , G01S19/254 , G01S13/88
摘要： A satellite system operates at altitudes between 100 and 350 km relying on vehicles including a self-sustaining ion engine to counteract atmospheric drag to maintain near-constant orbit dynamics. The system operates at altitudes that are substantially lower than traditional satellites, reducing size, weight and cost of the vehicles and their constituent subsystems such as optical imagers, radars, and radio links. The system can include a large number of lower cost, mass, and altitude vehicles, enabling revisit times substantially shorter than previous satellite systems. The vehicles spend their orbit at low altitude, high atmospheric density conditions that have heretofore been virtually impossible to consider for stable orbits. Short revisit times at low altitudes enable near-real time imaging at high resolution and low cost. At such altitudes, the system has no impact on space junk issues of traditional LEO orbits, and is self-cleaning in that space junk or disabled craft will de-orbit.
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10.发明授权公开(公告)号：US11671169B2
公开(公告)日：2023-06-06
申请号：US16925081
申请日：2020-07-09
申请人： Skeyeon, Inc.
发明人： Dan Nobbe , Ronald E. Reedy
CPC分类号： H04B7/18513 , G01S19/254 , H04B7/18534 , H04W84/06 , G01S13/88
摘要： A satellite system operates at altitudes between 100 and 350 km relying on vehicles including a self-sustaining ion engine to counteract atmospheric drag to maintain near-constant orbit dynamics. The system operates at altitudes that are substantially lower than traditional satellites, reducing size, weight and cost of the vehicles and their constituent subsystems such as optical imagers, radars, and radio links. The system can include a large number of lower cost, mass, and altitude vehicles, enabling revisit times substantially shorter than previous satellite systems. The vehicles spend their orbit at low altitude, high atmospheric density conditions that have heretofore been virtually impossible to consider for stable orbits. Short revisit times at low altitudes enable near-real time imaging at high resolution and low cost. At such altitudes, the system has no impact on space junk issues of traditional LEO orbits, and is self-cleaning in that space junk or disabled craft will de-orbit.
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