EA201490366A8 - Модульная центральная конструкция для совместного запуска космических летательных аппаратов - Google Patents
Модульная центральная конструкция для совместного запуска космических летательных аппаратовInfo
- Publication number
- EA201490366A8 EA201490366A8 EA201490366A EA201490366A EA201490366A8 EA 201490366 A8 EA201490366 A8 EA 201490366A8 EA 201490366 A EA201490366 A EA 201490366A EA 201490366 A EA201490366 A EA 201490366A EA 201490366 A8 EA201490366 A8 EA 201490366A8
- Authority
- EA
- Eurasian Patent Office
- Prior art keywords
- central structure
- cylinder
- space aircraft
- modular central
- spacecraft
- Prior art date
Links
Classifications
-
- 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
-
- 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
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
- B64G1/1085—Swarms and constellations
-
- 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
- B64G1/223—Modular spacecraft 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
- B64G1/402—Propellant tanks; Feeding propellants
-
- 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
- B64G1/643—Interstage or payload connectors for arranging multiple satellites in a single launcher
-
- 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
- B64G1/402—Propellant tanks; Feeding propellants
- B64G1/4022—Arrangements of tanks in or on spacecraft
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Astronomy & Astrophysics (AREA)
- General Physics & Mathematics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Moulding By Coating Moulds (AREA)
- Mutual Connection Of Rods And Tubes (AREA)
- Details Of Aerials (AREA)
Abstract
В заявке описан космический летательный аппарат, содержащий верхнюю центральную конструкцию или нижнюю центральную конструкцию. Верхняя центральная конструкция может содержать верхний цилиндр для поддержки верхнего КЛА в кассетной стартовой конфигурации. Нижняя центральная конструкция может содержать нижний цилиндр для поддержки нижнего космического летательного аппарата с верхним цилиндром, смонтированным поверх нижнего цилиндра. Верхний цилиндр может обладать внутренним диаметром, который может быть, по существу, равен внутреннему диаметру нижнего цилиндра.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/781,373 US9027889B2 (en) | 2013-02-28 | 2013-02-28 | Modular core structure for dual-manifest spacecraft launch |
Publications (4)
Publication Number | Publication Date |
---|---|
EA201490366A1 EA201490366A1 (ru) | 2014-08-29 |
EA201490366A8 true EA201490366A8 (ru) | 2016-01-29 |
EA031358B1 EA031358B1 (ru) | 2018-12-28 |
EA031358B9 EA031358B9 (ru) | 2019-06-28 |
Family
ID=50272274
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EA201490366A EA031358B9 (ru) | 2013-02-28 | 2014-02-27 | Модульная центральная конструкция для сдвоенного запуска космических летательных аппаратов |
Country Status (3)
Country | Link |
---|---|
US (1) | US9027889B2 (ru) |
EP (1) | EP2772441B1 (ru) |
EA (1) | EA031358B9 (ru) |
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US9027889B2 (en) * | 2013-02-28 | 2015-05-12 | The Boeing Comapny | Modular core structure for dual-manifest spacecraft launch |
US20150001344A1 (en) * | 2013-06-26 | 2015-01-01 | Raytheon Company | Satellite positioning system |
US9669948B2 (en) * | 2013-07-24 | 2017-06-06 | Lockheed Martin Corporation | Side-by-side dual-launch arrangement with improved payload compatibility |
US9242743B2 (en) * | 2013-10-10 | 2016-01-26 | Space Systems/Loral, Llc | Side-by-side multiple launch configuration |
FR3041940B1 (fr) | 2015-10-02 | 2018-07-13 | Airbus Defence And Space Sas | Satellite a corps principal cylindrique, empilement comprenant un tel satellite et ensemble de lancement pour un tel satellite |
FR3041939B1 (fr) | 2015-10-02 | 2017-10-20 | Airbus Defence & Space Sas | Satellite comprenant un instrument optique de prise de vue |
RU2648520C2 (ru) * | 2016-05-20 | 2018-03-26 | Акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнёва" | Космическая платформа |
US10306984B2 (en) * | 2016-08-30 | 2019-06-04 | The Boeing Company | Toroidal support structures |
US11286062B1 (en) | 2016-10-27 | 2022-03-29 | Space Systems/Loral, Llc | Spacecraft exoskeleton truss structure |
US10407189B1 (en) | 2016-10-27 | 2019-09-10 | Space Systems/Loral, Llc | Spacecraft exoskeleton truss structure |
US11254453B2 (en) * | 2016-11-14 | 2022-02-22 | Space Systems/Loral, Llc | Smallsat payload configuration |
US10351268B2 (en) * | 2016-12-08 | 2019-07-16 | The Boeing Company | Systems and methods for deploying spacecraft |
RU2658262C1 (ru) * | 2017-02-28 | 2018-06-19 | Акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнёва" | Способ сборки космического аппарата |
US11072441B2 (en) * | 2017-03-03 | 2021-07-27 | Northrop Grumman Systems Corporation | Stackable spacecraft |
US10633123B2 (en) | 2017-04-05 | 2020-04-28 | Space Systems/Loral, Llc | Exoskeletal launch support structure |
US10479534B1 (en) * | 2017-04-14 | 2019-11-19 | Space Systems/Loral, Llc | Rotatable stacked spacecraft |
RU2022100790A (ru) * | 2017-07-21 | 2022-02-11 | Нортроп Грамман Системз Корпорейшн | Обслуживающие устройства космического аппарата и соответствующие узлы, системы и способы |
US11878820B1 (en) * | 2019-05-14 | 2024-01-23 | Space Exploration Technologies Corp. | Method for stacking, securing, and releasing a spacecraft stack assembly from a rocket |
US11787572B1 (en) * | 2019-05-14 | 2023-10-17 | Space Exploration Technologies Corp. | Spacecraft stack assembly configured for stacking, securing, and releasing spacecraft |
US11345489B2 (en) | 2019-08-19 | 2022-05-31 | The Boeing Company | Satellite dispenser and method of supporting a plurality of satellites |
US11794927B2 (en) | 2019-08-28 | 2023-10-24 | The Boeing Company | Additively manufactured spacecraft panel |
RU2729148C1 (ru) * | 2019-12-20 | 2020-08-04 | Акционерное общество «Информационные спутниковые системы» имени академика М.Ф.Решетнёва» | Модуль полезной нагрузки космического аппарата |
WO2021212355A1 (zh) * | 2020-04-22 | 2021-10-28 | 中国科学院微小卫星创新研究院 | 卫星构型及其分离方法 |
US11802606B2 (en) | 2020-05-18 | 2023-10-31 | The Boeing Company | Planate dynamic isolator |
US11827389B2 (en) | 2020-05-18 | 2023-11-28 | The Boeing Company | Additively manufactured satellite |
CN111942620A (zh) * | 2020-08-11 | 2020-11-17 | 中国科学院微小卫星创新研究院 | 电推进贮箱支撑结构及其总装方法 |
CN111891397A (zh) * | 2020-08-12 | 2020-11-06 | 中国科学院微小卫星创新研究院 | 小型高轨卫星的一箭多星自串联发射结构 |
US20220106063A1 (en) * | 2020-10-04 | 2022-04-07 | Omniteq, Llc | Satellite deployer method, system, and apparatus |
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CN112572840A (zh) * | 2020-12-14 | 2021-03-30 | 兰州空间技术物理研究所 | 一种电推进系统贮供单元及其制造方法 |
RU2758656C1 (ru) * | 2020-12-16 | 2021-11-01 | Федеральное государственное автономное образовательное учреждение высшего образования «Южно-Уральский государственный университет (национальный исследовательский университет)» ФГАОУ ВО «ЮУрГУ (НИУ)» | Космический аппарат для доставки полезного груза на космическое тело с малым гравитационным полем |
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-
2013
- 2013-02-28 US US13/781,373 patent/US9027889B2/en active Active
-
2014
- 2014-02-24 EP EP14156420.3A patent/EP2772441B1/en active Active
- 2014-02-27 EA EA201490366A patent/EA031358B9/ru not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
US20140239125A1 (en) | 2014-08-28 |
EP2772441A2 (en) | 2014-09-03 |
US9027889B2 (en) | 2015-05-12 |
EP2772441A3 (en) | 2015-07-08 |
EA031358B1 (ru) | 2018-12-28 |
EA201490366A1 (ru) | 2014-08-29 |
EP2772441B1 (en) | 2018-04-11 |
EA031358B9 (ru) | 2019-06-28 |
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TH4A | Publication of the corrected specification to eurasian patent | ||
MM4A | Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s) |
Designated state(s): AM AZ BY KG TJ TM |