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 PDF

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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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Russia
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cable
orbital
descent
orbital station
station
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RU2011144048/11A
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Russian (ru)
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RU2497729C2 (en
Inventor
Валерий Иванович Щербаков
Алексей Петрович Софьин
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Федеральное государственное военное образовательное учреждение высшего профессионального образования "Военно-космическая академия имени А.Ф. Можайского" Министерства обороны Российской Федерации
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Application filed by Федеральное государственное военное образовательное учреждение высшего профессионального образования "Военно-космическая академия имени А.Ф. Можайского" Министерства обороны Российской Федерации filed Critical Федеральное государственное военное образовательное учреждение высшего профессионального образования "Военно-космическая академия имени А.Ф. Можайского" Министерства обороны Российской Федерации
Priority to RU2011144048/11A priority Critical patent/RU2497729C2/en
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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.

Claims (1)

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.
RU2011144048/11A 2011-10-31 2011-10-31 Method of delivery of lander from orbital station to earth based on passive deployment of space cable system RU2497729C2 (en)

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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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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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RU2497729C2 RU2497729C2 (en) 2013-11-10

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Families Citing this family (2)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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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Effective date: 20141101