PL3313734T3 - Satelita z cylindrycznym korpusem głównym, stos zawierający takiego satelitę i zespół do wystrzeliwania dla takiego satelity - Google Patents
Satelita z cylindrycznym korpusem głównym, stos zawierający takiego satelitę i zespół do wystrzeliwania dla takiego satelityInfo
- Publication number
- PL3313734T3 PL3313734T3 PL16788161T PL16788161T PL3313734T3 PL 3313734 T3 PL3313734 T3 PL 3313734T3 PL 16788161 T PL16788161 T PL 16788161T PL 16788161 T PL16788161 T PL 16788161T PL 3313734 T3 PL3313734 T3 PL 3313734T3
- Authority
- PL
- Poland
- Prior art keywords
- satellite
- stack
- main body
- cylindrical main
- launch assembly
- Prior art date
Links
Classifications
-
- 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
-
- 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
- B64G1/1021—Earth observation satellites
-
- 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
- B64G1/1021—Earth observation satellites
- B64G1/1028—Earth observation satellites using optical means for mapping, surveying or detection, e.g. of intelligence
-
- 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
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/285—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using momentum wheels
-
- 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
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/286—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using control momentum gyroscopes (CMGs)
-
- 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
- B64G1/642—Clamps, e.g. Marman clamps
-
- 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
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
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)
- Radar, Positioning & Navigation (AREA)
- Mechanical Engineering (AREA)
- Evolutionary Computation (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Telescopes (AREA)
- Photovoltaic Devices (AREA)
- Details Of Aerials (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1559386A FR3041940B1 (fr) | 2015-10-02 | 2015-10-02 | Satellite a corps principal cylindrique, empilement comprenant un tel satellite et ensemble de lancement pour un tel satellite |
| PCT/FR2016/052507 WO2017055770A1 (fr) | 2015-10-02 | 2016-09-30 | Satellite à corps principal cylindrique, empilement comprenant un tel satellite et ensemble de lancement pour un tel satellite |
| EP16788161.4A EP3313734B1 (fr) | 2015-10-02 | 2016-09-30 | Satellite à corps principal cylindrique, empilement comprenant un tel satellite et ensemble de lancement pour un tel satellite |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| PL3313734T3 true PL3313734T3 (pl) | 2019-01-31 |
Family
ID=55646666
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PL16788161T PL3313734T3 (pl) | 2015-10-02 | 2016-09-30 | Satelita z cylindrycznym korpusem głównym, stos zawierający takiego satelitę i zespół do wystrzeliwania dla takiego satelity |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US10689133B2 (pl) |
| EP (1) | EP3313734B1 (pl) |
| ES (1) | ES2690991T3 (pl) |
| FR (1) | FR3041940B1 (pl) |
| PL (1) | PL3313734T3 (pl) |
| WO (1) | WO2017055770A1 (pl) |
Families Citing this family (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8915472B2 (en) * | 2012-05-11 | 2014-12-23 | The Boeing Company | Multiple space vehicle launch system |
| US9180984B2 (en) | 2012-05-11 | 2015-11-10 | The Boeing Company | Methods and apparatus for performing propulsion operations using electric propulsion systems |
| FR3041939B1 (fr) * | 2015-10-02 | 2017-10-20 | Airbus Defence & Space Sas | Satellite comprenant un instrument optique de prise de vue |
| US10351268B2 (en) * | 2016-12-08 | 2019-07-16 | The Boeing Company | Systems and methods for deploying spacecraft |
| US11072441B2 (en) * | 2017-03-03 | 2021-07-27 | Northrop Grumman Systems Corporation | Stackable spacecraft |
| US10981679B2 (en) | 2017-08-04 | 2021-04-20 | Rocket Lab Usa, Inc. | Satellite deployer door release mechanism |
| GB2564734B (en) * | 2017-10-18 | 2019-07-10 | Ellinghaus Frank | Panelsat, an agile satellite with fuel free attitude control |
| KR102002306B1 (ko) * | 2018-01-08 | 2019-07-22 | 주식회사 버츄얼랩 | 큐브위성 우주 분리장치 |
| JP2021510650A (ja) * | 2018-01-22 | 2021-04-30 | ルアク・シュヴァイツ・アクチェンゲゼルシャフトRuag Schweiz Ag | ペイロードキャリアアセンブリ |
| IL257491B (en) * | 2018-02-12 | 2021-02-28 | Israel Aerospace Ind Ltd | A space vehicle deploys |
| IL258729B (en) | 2018-04-16 | 2021-12-01 | Israel Aerospace Ind Ltd | Nano-satellite |
| WO2019223984A1 (en) * | 2018-05-24 | 2019-11-28 | The European Union, Represented By The European Commission | Efficient satellite structure concept for single or stacking multiple launches |
| US11560243B2 (en) | 2019-02-22 | 2023-01-24 | Blue Origin, Llc | Spacecraft multifunction connecting mechanisms including interchangeable port opening docking mechanisms, and associated systems and methods |
| US11565628B2 (en) * | 2019-03-29 | 2023-01-31 | Blue Origin, Llc | Spacecraft with increased cargo capacities, and associated systems and methods |
| CN110861785B (zh) * | 2019-11-30 | 2021-06-08 | 中国人民解放军战略支援部队航天工程大学 | 一种光学成像卫星 |
| US11987395B2 (en) | 2021-06-07 | 2024-05-21 | Blue Origin, Llc | Thrusting rails for launch vehicles, and associated systems and methods |
| US12378008B2 (en) | 2023-04-20 | 2025-08-05 | Maxar Space Llc | Solar array spring elements for stacking spacecraft |
| FR3151300B1 (fr) * | 2023-07-17 | 2025-07-18 | Airbus Defence & Space Sas | Procédé et système spatial pour l'éjection d'un empilement de satellites |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4009851A (en) * | 1974-12-23 | 1977-03-01 | Rca Corporation | Spacecraft structure |
| ES2046021T3 (es) * | 1990-02-26 | 1994-01-16 | Aerospatiale | Satelite de observacion de tipo geoestacionario con sistema de maniobra de apogeo de ergoles liquidos y con varias toberas. |
| US5169094A (en) * | 1990-02-26 | 1992-12-08 | Aerospatiale Societe Nationale Industrielle | Geostationary earth observation satellite incorporating liquid propellant apogee maneuver system and hollow antennas |
| US5337980A (en) * | 1992-09-21 | 1994-08-16 | General Electric Co. | Spacecraft-to-launch-vehicle transition |
| EP1190948A3 (de) * | 2000-09-22 | 2002-10-16 | Astrium GmbH | Vorrichtung zum Bergen von Raumflugkörpern |
| JP4705172B2 (ja) * | 2005-10-06 | 2011-06-22 | エアドス カサ エスパシオ ソシエダ リミタダ | 打ち上げロケットと衛星を連結および分離する装置 |
| US7840180B2 (en) * | 2006-12-22 | 2010-11-23 | The Boeing Company | Molniya orbit satellite systems, apparatus, and methods |
| US8016240B2 (en) * | 2007-03-29 | 2011-09-13 | The Boeing Company | Satellites and satellite fleet implementation methods and apparatus |
| FR2932576B1 (fr) * | 2008-06-13 | 2013-02-15 | Thales Sa | Ensemble multi-instruments embarque ultra-stable. |
| FR2939912B1 (fr) * | 2008-12-12 | 2011-04-15 | Thales Sa | Ensemble de support d'un miroir secondaire d'un engin spatial d'observation de haute stabilite et a faible inertie mecanique |
| FR2959490B1 (fr) * | 2010-04-28 | 2012-07-13 | Astrium Sas | Satellite a structure simplifiee, allegee et economique, et son procede de mise en oeuvre |
| EP4462601A3 (en) * | 2010-12-15 | 2025-02-19 | Planet Labs PBC | Integrated antenna system for imaging microsatellites |
| EP2489593A1 (en) * | 2011-02-21 | 2012-08-22 | European Space Agency | Earth observation satellite, satellite system, and launching system for launching satellites |
| US8789797B2 (en) * | 2012-02-23 | 2014-07-29 | Alliant Techsystems Inc. | Payload adapters including antenna assemblies, satellite assemblies and related systems and methods |
| US8939409B2 (en) | 2012-05-07 | 2015-01-27 | The Johns Hopkins University | Adaptor system for deploying small satellites |
| US9027889B2 (en) * | 2013-02-28 | 2015-05-12 | The Boeing Comapny | Modular core structure for dual-manifest spacecraft launch |
| FR3041939B1 (fr) * | 2015-10-02 | 2017-10-20 | Airbus Defence & Space Sas | Satellite comprenant un instrument optique de prise de vue |
-
2015
- 2015-10-02 FR FR1559386A patent/FR3041940B1/fr not_active Expired - Fee Related
-
2016
- 2016-09-30 WO PCT/FR2016/052507 patent/WO2017055770A1/fr not_active Ceased
- 2016-09-30 US US15/764,678 patent/US10689133B2/en active Active
- 2016-09-30 ES ES16788161.4T patent/ES2690991T3/es active Active
- 2016-09-30 EP EP16788161.4A patent/EP3313734B1/fr active Active
- 2016-09-30 PL PL16788161T patent/PL3313734T3/pl unknown
Also Published As
| Publication number | Publication date |
|---|---|
| US20180265227A1 (en) | 2018-09-20 |
| ES2690991T3 (es) | 2018-11-23 |
| EP3313734A1 (fr) | 2018-05-02 |
| FR3041940A1 (fr) | 2017-04-07 |
| WO2017055770A1 (fr) | 2017-04-06 |
| FR3041940B1 (fr) | 2018-07-13 |
| EP3313734B1 (fr) | 2018-09-26 |
| US10689133B2 (en) | 2020-06-23 |
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