RU2011144048A - METHOD OF DELIVERY FROM THE ORBITAL STATION TO THE LAND OF THE RELEASED MACHINE BASED ON THE USE OF PASSIVE DEPLOYMENT OF THE SPACE ROPE SYSTEM - Google Patents
METHOD OF DELIVERY FROM THE ORBITAL STATION TO THE LAND OF THE RELEASED MACHINE BASED ON THE USE OF PASSIVE DEPLOYMENT OF THE SPACE ROPE SYSTEM Download PDFInfo
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- RU2011144048A RU2011144048A RU2011144048/11A RU2011144048A RU2011144048A RU 2011144048 A RU2011144048 A RU 2011144048A RU 2011144048/11 A RU2011144048/11 A RU 2011144048/11A RU 2011144048 A RU2011144048 A RU 2011144048A RU 2011144048 A RU2011144048 A RU 2011144048A
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- Prior art keywords
- cable
- orbital
- descent
- orbital station
- station
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- Electric Cable Installation (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Laying Of Electric Cables Or Lines Outside (AREA)
Abstract
Способ доставки с орбитальной станции на Землю спускаемого аппарата с использованием пассивного развертывания космической тросовой системы, включающий расстыковку двух соединенных тросом объектов, сообщение спускаемому аппарату начальной скорости расхождения, свободный выпуск троса при удалении спускаемого аппарата, фиксацию длины троса в конце реверсного участка, попутное маятниковое движение и отрезание троса в момент прохождения спускаемым аппаратом линии местной вертикали орбитальной станции, отличающийся тем, что отделение спускаемого аппарата производят против вектора орбитальной скорости без управления силой натяжения троса при удалении спускаемого аппарата, а также производят выборку свободного троса на реверсном участке траектории.A method of delivering a descent vehicle from an orbital station to Earth using the passive deployment of a space cable system, including undocking two objects connected by a cable, informing the descent vehicle of the initial speed of divergence, free release of the cable when the descent device is removed, fixing the cable length at the end of the reverse section, associated pendulum movement and cutting the cable at the moment the lander passes the local vertical line of the orbital station, characterized in that the compartment produced against the started-up apparatus of the orbital velocity vector control without power cable tension upon removal of the landing device, and also produce free cable sample into reverse trajectory.
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Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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RU2011144048/11A RU2497729C2 (en) | 2011-10-31 | 2011-10-31 | Method of delivery of lander from orbital station to earth based on passive deployment of space cable system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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RU2011144048/11A RU2497729C2 (en) | 2011-10-31 | 2011-10-31 | Method of delivery of lander from orbital station to earth based on passive deployment of space cable system |
Publications (2)
Publication Number | Publication Date |
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RU2011144048A true RU2011144048A (en) | 2013-05-10 |
RU2497729C2 RU2497729C2 (en) | 2013-11-10 |
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Application Number | Title | Priority Date | Filing Date |
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RU2011144048/11A RU2497729C2 (en) | 2011-10-31 | 2011-10-31 | Method of delivery of lander from orbital station to earth based on passive deployment of space cable system |
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RU (1) | RU2497729C2 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2564930C1 (en) * | 2014-03-12 | 2015-10-10 | Федеральное государственное казенное военное образовательное учреждение высшего профессионального образования "Военно-космическая академия имени А.Ф. Можайского" Министерства обороны Российской Федерации | Deployment of space rope system at delivery of lander from orbital station to ground |
RU2586920C1 (en) * | 2015-01-26 | 2016-06-10 | Федеральное государственное казенное военное образовательное учреждение высшего профессионального образования "Военно-космическая академия имени А.Ф. Можайского" Министерства обороны Российской Федерации | Method of manoeuvring deviation of spacecraft on orbit from collision with other bodies |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SU137337A1 (en) * | 1960-03-09 | 1960-11-30 | нов С.А. Емель | Device for protection from drift of drift net leader |
SU1235818A1 (en) * | 1984-12-06 | 1986-06-07 | Дальневосточный Ордена Трудового Красного Знамени Политехнический Институт Им.В.В.Куйбышева | Device for controlling drive of ship winch |
RU2112715C1 (en) * | 1996-10-03 | 1998-06-10 | Ракетно-космическая корпорация "Энергия" им.С.П.Королева | Method of deployment of orbital cable system |
US6913224B2 (en) * | 2003-09-29 | 2005-07-05 | Dana R. Johansen | Method and system for accelerating an object |
US7503526B1 (en) * | 2005-09-23 | 2009-03-17 | Taylor Thomas C | Space transportation node including tether system |
US8052092B2 (en) * | 2009-01-30 | 2011-11-08 | The Boeing Company | Method and apparatus for satellite orbital change using space debris |
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2011
- 2011-10-31 RU RU2011144048/11A patent/RU2497729C2/en not_active IP Right Cessation
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RU2497729C2 (en) | 2013-11-10 |
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MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20141101 |