EA201300451A1 - Система вывода на орбиту нескольких космических аппаратов - Google Patents

Система вывода на орбиту нескольких космических аппаратов

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Publication number
EA201300451A1
EA201300451A1 EA201300451A EA201300451A EA201300451A1 EA 201300451 A1 EA201300451 A1 EA 201300451A1 EA 201300451 A EA201300451 A EA 201300451A EA 201300451 A EA201300451 A EA 201300451A EA 201300451 A1 EA201300451 A1 EA 201300451A1
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EA
Eurasian Patent Office
Prior art keywords
spacecraft
electric
orbit
conclusion
space devices
Prior art date
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EA201300451A
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English (en)
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EA201300451A8 (ru
EA025867B1 (ru
Inventor
Ричард В. Астон
Анна М. Томзинская
Гленн Н. Кэплин
Original Assignee
Дзе Боинг Компани
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Application filed by Дзе Боинг Компани filed Critical Дзе Боинг Компани
Publication of EA201300451A1 publication Critical patent/EA201300451A1/ru
Publication of EA201300451A8 publication Critical patent/EA201300451A8/ru
Publication of EA025867B1 publication Critical patent/EA025867B1/ru

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/002—Launch systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/405—Ion or plasma engines
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/641—Interstage or payload connectors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/645—Separators
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays

Abstract

Система одновременного запуска нескольких космических аппаратов (10), которую можно адаптировать для размещения внутри области полезной нагрузки (20) обтекателя ракеты-носителя (14). Система запуска может состоять из первого космического аппарата (16), второго космического аппарата (18) с возможностью последующей пристыковки к первому космическому аппарату (16) и ориентированного относительно первого космического аппарата (16) таким образом, что при размещении внутри обтекателя (14) стартовая нагрузка первого космического аппарата (16) передается второму космическому аппарату (18) и выдерживается им. В определенных модификациях первый и второй космические аппараты (16, 18) могут быть оборудованы либо электрическим двигателем (40), либо гибридным химическим и электрическим двигателем (42). Использование электрического и гибридного электрического и химического двигателей (40, 42) позволяет второму космическому аппарату (18) выдерживать всю или значительную часть стартовой нагрузки первого космического аппарата (16), устраняя тем самым потребность в использовании дополнительной опорной конструкции.
EA201300451A 2012-05-11 2013-05-08 Система вывода на орбиту нескольких космических аппаратов EA025867B1 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201261646222P 2012-05-11 2012-05-11
US13/604,050 US8915472B2 (en) 2012-05-11 2012-09-05 Multiple space vehicle launch system

Publications (3)

Publication Number Publication Date
EA201300451A1 true EA201300451A1 (ru) 2013-12-30
EA201300451A8 EA201300451A8 (ru) 2016-01-29
EA025867B1 EA025867B1 (ru) 2017-02-28

Family

ID=48463738

Family Applications (1)

Application Number Title Priority Date Filing Date
EA201300451A EA025867B1 (ru) 2012-05-11 2013-05-08 Система вывода на орбиту нескольких космических аппаратов

Country Status (4)

Country Link
US (5) US8915472B2 (ru)
EP (2) EP2662287B1 (ru)
CN (2) CN103387058B (ru)
EA (1) EA025867B1 (ru)

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US8915472B2 (en) 2014-12-23
EA201300451A8 (ru) 2016-01-29
EP3578466A1 (en) 2019-12-11
US11286066B2 (en) 2022-03-29
EP3578466B1 (en) 2023-12-20
CN105775164A (zh) 2016-07-20
US20130299641A1 (en) 2013-11-14
EP2662287A1 (en) 2013-11-13
US20220127022A1 (en) 2022-04-28
CN103387058A (zh) 2013-11-13
US20160046397A1 (en) 2016-02-18
US9957068B2 (en) 2018-05-01
EP2662287B1 (en) 2020-04-29
US20180201396A1 (en) 2018-07-19
EA025867B1 (ru) 2017-02-28
US20150001348A1 (en) 2015-01-01
CN103387058B (zh) 2016-05-18

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