RU2010120889A - SATELLITE SYSTEM WITH ULTRA-HIGH SOLAR-SYNCHRONOUS ORBIT - Google Patents
SATELLITE SYSTEM WITH ULTRA-HIGH SOLAR-SYNCHRONOUS ORBIT Download PDFInfo
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- RU2010120889A RU2010120889A RU2010120889/11A RU2010120889A RU2010120889A RU 2010120889 A RU2010120889 A RU 2010120889A RU 2010120889/11 A RU2010120889/11 A RU 2010120889/11A RU 2010120889 A RU2010120889 A RU 2010120889A RU 2010120889 A RU2010120889 A RU 2010120889A
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Abstract
1. Спутниковая система на гелиоцентрической орбите, образующей солнечно-синхронную орбиту вокруг Земли, включающую гало-орбиты и другие орбиты, которые используют синхронизм с вращением Земли, характеризующаяся тем, что представляет собой спутниковую систему (3), которая позволяет выполнять любую из следующих услуг: наблюдение космического пространства, глобальное наблюдение и спутниковая связь, ! причем указанная спутниковая система вращается вокруг Солнца (5), но при этом вращается вокруг Земли, выполняя, по существу, круговое или эллиптическое движение вне сферы гравитационного поля Земли на расстоянии, по меньшей мере, несколько миллионов километров, при этом указанная круговая или эллиптическая орбитальная плоскость относительно Земли, по существу, является фиксированной, если наблюдать из системы координат, центром которой является Земля; ! при этом отношение между углом наклона орбиты и ее эксцентриситетом относительно эклиптических координат выбрано в соответствии с указанными услугами, причем с помощью одного спутника может быть одновременно охвачено, по существу, полушарие Земли, и, по существу, вся поверхность Земли может быть охвачена при размещении небольшого количества или трех указанных спутников (3) на равных расстояниях на указанной орбите. ! 2. Спутниковая система на гелиоцентрической орбите, образующей солнечно-синхронную орбиту вокруг Земли, по п.1, характеризующаяся тем, что отношение между углом наклона орбиты и ее эксцентриситетом относительно эклиптических координат составляет 1,73, что позволяет иметь постоянное расстояние от Земли. 1. A satellite system in a heliocentric orbit, forming a sun-synchronous orbit around the Earth, including halo orbits and other orbits that use synchronism with the rotation of the Earth, characterized in that it is a satellite system (3), which allows you to perform any of the following services : outer space observation, global observation and satellite communications,! wherein said satellite system rotates around the Sun (5), but rotates around the Earth, performing essentially circular or elliptical motion outside the sphere of the Earth’s gravitational field at a distance of at least several million kilometers, while said circular or elliptical orbital the plane relative to the Earth, in essence, is fixed, if you observe from a coordinate system whose center is the Earth; ! the ratio between the inclination angle of the orbit and its eccentricity relative to the ecliptic coordinates is chosen in accordance with the indicated services, moreover, with the help of one satellite, essentially the Earth’s hemisphere can be simultaneously covered, and essentially the entire Earth’s surface can be covered when placing a small the number or three of these satellites (3) at equal distances in the indicated orbit. ! 2. The satellite system in a heliocentric orbit, forming a sun-synchronous orbit around the Earth according to claim 1, characterized in that the ratio between the angle of inclination of the orbit and its eccentricity relative to the ecliptic coordinates is 1.73, which allows you to have a constant distance from the Earth.
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RU2010120889/11A RU2576643C2 (en) | 2010-05-24 | 2010-05-24 | Ultrahigh altitude sun synchronous orbit satellite system |
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RU2010120889/11A RU2576643C2 (en) | 2010-05-24 | 2010-05-24 | Ultrahigh altitude sun synchronous orbit satellite system |
Related Parent Applications (1)
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RU2007102045/11A Division RU2007102045A (en) | 2004-06-22 | 2004-06-22 | SATELLITE SYSTEM WITH ULTRA-HIGH SOLAR-SYNCHRONOUS ORBIT |
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RU2010120889A true RU2010120889A (en) | 2011-11-27 |
RU2576643C2 RU2576643C2 (en) | 2016-03-10 |
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RU2010120889/11A RU2576643C2 (en) | 2010-05-24 | 2010-05-24 | Ultrahigh altitude sun synchronous orbit satellite system |
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Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
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RU2752753C1 (en) * | 2020-08-14 | 2021-08-02 | Игорь Николаевич Пантелеймонов | Method for organising communication with objects located in orbit and on surface of planet or satellite of planet, and deep space communication system for implementation of method |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
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US3706037A (en) * | 1970-02-25 | 1972-12-12 | Bell Telephone Labor Inc | Communication satellite system |
US5183225A (en) * | 1989-01-09 | 1993-02-02 | Forward Robert L | Statite: spacecraft that utilizes sight pressure and method of use |
RU2003136C1 (en) * | 1991-07-11 | 1993-11-15 | Институт земного магнетизма, ионосферы и распространени радиоволн РАН | Method of prediction of parameters of solar wind at level of orbit of the earth |
SU1764523A3 (en) * | 1991-10-04 | 1992-09-23 | Bryzhinskij Yurij V | Energy converter |
US5582367A (en) * | 1992-06-02 | 1996-12-10 | Mobile Communications Holdings, Inc. | Elliptical orbit satellite, system, and deployment with controllable coverage characteristics |
RU2155447C1 (en) * | 1999-08-09 | 2000-08-27 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" им.С.П.Королева" | Satellite system for data transmission between customer satellites and ground station |
JP4472240B2 (en) * | 2002-08-28 | 2010-06-02 | Nec東芝スペースシステム株式会社 | Communication satellite system |
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RU2576643C2 (en) | 2016-03-10 |
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