RU2010119972A - METHOD FOR REMOVING SPACE DEBR FROM USE OF USEFUL LOADS ON THE BASIS OF USING THE SEPARATED PART OF A ROCKET-CARRIER, AN ACCELERATION UNIT AND A DEVICE FOR ITS IMPLEMENTATION - Google Patents
METHOD FOR REMOVING SPACE DEBR FROM USE OF USEFUL LOADS ON THE BASIS OF USING THE SEPARATED PART OF A ROCKET-CARRIER, AN ACCELERATION UNIT AND A DEVICE FOR ITS IMPLEMENTATION Download PDFInfo
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- RU2010119972A RU2010119972A RU2010119972/11A RU2010119972A RU2010119972A RU 2010119972 A RU2010119972 A RU 2010119972A RU 2010119972/11 A RU2010119972/11 A RU 2010119972/11A RU 2010119972 A RU2010119972 A RU 2010119972A RU 2010119972 A RU2010119972 A RU 2010119972A
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Abstract
1. Способ увода космического мусора (КМ) с орбит полезных нагрузок на основе приложения импульса маневра к отделяющейся части (ОЧ) ступени ракеты-носителя (РН), разгонного блока (РБ) для увода на орбиту утилизации на основе использования невыработанных запасов жидкого топлива после разрыва механической связи с полезной нагрузкой, отличающийся тем, что перед уводом ОЧ ступени РН, РБ на орбиту утилизации осуществляют дальнее наведение ОЧ ступени РН, РБ в район встречи с выбранным для увода с орбиты КМ, а этап ближнего наведения ОЧ ступени РН, РБ с выбранным КМ осуществляют с помощью отделяемого от ОЧ ступени РН, РБ малоразмерного космического буксира (МКБ), связанного механической связью с ОЧ ступени РН, РБ тросом, осуществляют стыковку МКБ с КМ, после прилагают тормозной импульс к ОЧ ступени РН, РБ для увода связки «ОЧ ступени РН, РБ-трос-МКБ-КМ» на орбиту утилизации. ! 2. Способ по п.1, отличающийся тем, что запасы остатков жидких невыработанных компонентов ракетного топлива в баках окислителя и горючего в ОЧ ступени РН, РБ определяют исходя из затрат на маневр дальнего наведения и транспортировки связки «ОЧ ступени РН, РБ-трос-МКБ-КМ» на орбиту утилизации. ! 3. Способ по п.1, отличающийся тем, что при разматывании троса, обеспечивают линейную скорость его схода с барабана на 2-3% больше относительной скорости сближения МКБ и КМ, при торможении МКБ перед стыковкой с КМ, скорость разматывания троса снижают в соответствии со снижением относительной скорости, а перед приложением тормозного импульса для перевода связки «ОЧ ступени РН-трос-МКБ-КМ» на орбиту утилизации осуществляют выбор провисания троса. ! 4. Устройство для реа� 1. A method of removing space debris (CM) from the orbits of payloads based on the application of a maneuver impulse to the separating part (OCh) of the launch vehicle (LV) stage, booster block (RB) for transfer to the orbit of disposal based on the use of undeveloped reserves of liquid fuel after rupture of the mechanical connection with the payload, characterized in that before the launch of the VL stage of the LV, RB into the disposal orbit, the VL stage of the LV, RB is distantly guided to the meeting area with the KM selected for removal from the orbit, and the stage of the near guidance of the VL stage of the LV, RB with the selected CM, the small-sized space tug (MCB) detachable from the OCh stage of the LV, RB connected by mechanical connection with the OCh stage of the PH, RB by a cable, dock the ICB with the KM, then apply a braking impulse to the OCh stage of the PH, RB to remove the ligament “OCH of the launch vehicle stage, RB-cable-MKB-KM” into orbit of disposal. ! 2. The method according to claim 1, characterized in that the reserves of residual liquid undeveloped components of rocket fuel in the oxidizer and fuel tanks in the PH stage of the launch vehicle, RB are determined based on the cost of maneuvering the long-range guidance and transportation of the bundle of “PH stage of the launch vehicle, RB-cable- ICD-KM ”into orbit of disposal. ! 3. The method according to claim 1, characterized in that when unwinding the cable, provide a linear speed of its descent from the drum is 2-3% higher than the relative speed of convergence of MKB and KM, when braking MKB before docking with KM, the speed of unwinding of the cable is reduced in accordance with a decrease in the relative speed, and before applying the braking impulse to transfer the bunch of “OCH stages RN-cable-MKB-KM” to the disposal orbit, the cable sagging is selected. ! 4. Device for real
Claims (4)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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RU2010119972/11A RU2462399C2 (en) | 2010-05-18 | 2010-05-18 | Method of space refuse withdrawal from payload orbit exploiting carrier rocket separated part and accelerating unit, and device to this end |
Applications Claiming Priority (1)
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RU2010119972/11A RU2462399C2 (en) | 2010-05-18 | 2010-05-18 | Method of space refuse withdrawal from payload orbit exploiting carrier rocket separated part and accelerating unit, and device to this end |
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RU2010119972A true RU2010119972A (en) | 2011-11-27 |
RU2462399C2 RU2462399C2 (en) | 2012-09-27 |
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RU2010119972/11A RU2462399C2 (en) | 2010-05-18 | 2010-05-18 | Method of space refuse withdrawal from payload orbit exploiting carrier rocket separated part and accelerating unit, and device to this end |
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Cited By (1)
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RU2559392C1 (en) * | 2014-04-18 | 2015-08-10 | Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт машиностроения" (ФГУП ЦНИИмаш) | Removal of non-functional spacecraft from geostationary orbit |
RU2643020C1 (en) * | 2016-09-06 | 2018-01-29 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Омский государственный технический университет" | Method for conducting flight development tests of autonomous docking module for cleaning orbits from space debris |
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RU2040448C1 (en) * | 1992-02-04 | 1995-07-25 | Головное конструкторское бюро Научно-производственного объединения им.акад.С.П.Королева | Space vehicle for cleaning space of foreign matter |
RU2040449C1 (en) * | 1992-03-13 | 1995-07-25 | Головное конструкторское бюро научно-производственного объединения "Энергия" им.акад.С.П.Королева | Apparatus for cleaning space of foreign matter |
RU2092408C1 (en) * | 1993-11-09 | 1997-10-10 | Ракетно-космическая корпорация "Энергия" им.С.П.Королева | Space vehicle for cleaning space from garbage |
RU2141436C1 (en) * | 1998-10-14 | 1999-11-20 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" им.С.П.Королева" | Space vehicle for cleaning space from passive space vehicles and their fragments |
US7070151B2 (en) * | 2004-01-09 | 2006-07-04 | Iostar Corporation | In orbit space transportation and recovery system |
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Cited By (2)
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CN107651224A (en) * | 2017-07-04 | 2018-02-02 | 上海宇航系统工程研究所 | Substep Racemization control method based on monosystem rope tie point to Spatial Instability target |
CN107651224B (en) * | 2017-07-04 | 2021-03-09 | 上海宇航系统工程研究所 | Step-by-step despinning control method for space instability target based on single-rope connecting point |
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