JP5372934B2 - ペイロード中心構成を有する宇宙船 - Google Patents
ペイロード中心構成を有する宇宙船 Download PDFInfo
- Publication number
- JP5372934B2 JP5372934B2 JP2010523014A JP2010523014A JP5372934B2 JP 5372934 B2 JP5372934 B2 JP 5372934B2 JP 2010523014 A JP2010523014 A JP 2010523014A JP 2010523014 A JP2010523014 A JP 2010523014A JP 5372934 B2 JP5372934 B2 JP 5372934B2
- Authority
- JP
- Japan
- Prior art keywords
- spacecraft
- equipment rooms
- rooms
- antenna
- configuration
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000004880 explosion Methods 0.000 claims description 5
- 239000002828 fuel tank Substances 0.000 claims description 5
- 230000003287 optical effect Effects 0.000 claims 1
- 238000004891 communication Methods 0.000 description 12
- 238000000034 method Methods 0.000 description 10
- 238000010586 diagram Methods 0.000 description 5
- 230000008569 process Effects 0.000 description 5
- 238000003860 storage Methods 0.000 description 4
- 238000012545 processing Methods 0.000 description 3
- 239000000446 fuel Substances 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 101000860173 Myxococcus xanthus C-factor Proteins 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 238000003491 array Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- 230000036541 health Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000032258 transport Effects 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
- 239000002759 woven fabric Substances 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
- H01Q1/288—Satellite antennas
-
- 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
- B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
-
- 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
- B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
- B64G1/2221—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state characterised by the manner of deployment
- B64G1/2222—Folding
- B64G1/2224—Folding about multiple axes
-
- 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
- B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
- B64G1/2221—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state characterised by the manner of deployment
- B64G1/2226—Telescoping
-
- 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
- B64G1/244—Spacecraft control 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
- B64G1/401—Liquid propellant rocket 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
- B64G1/40—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
- B64G1/42—Arrangements or adaptations of power supply systems
- B64G1/428—Power distribution and management
-
- 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
-
- 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
- B64G1/46—Arrangements or adaptations of devices for control of environment or living conditions
- B64G1/50—Arrangements or adaptations of devices for control of environment or living conditions for temperature control
-
- 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
- B64G1/52—Protection, safety or emergency devices; Survival aids
- B64G1/54—Protection against radiation
-
- 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
- B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Physics & Mathematics (AREA)
- Chemical & Material Sciences (AREA)
- Astronomy & Astrophysics (AREA)
- Toxicology (AREA)
- General Physics & Mathematics (AREA)
- Life Sciences & Earth Sciences (AREA)
- Combustion & Propulsion (AREA)
- Environmental Sciences (AREA)
- Automation & Control Theory (AREA)
- Radar, Positioning & Navigation (AREA)
- Emergency Medicine (AREA)
- Biodiversity & Conservation Biology (AREA)
- Environmental & Geological Engineering (AREA)
- Critical Care (AREA)
- Sustainable Development (AREA)
- Power Engineering (AREA)
- Plasma & Fusion (AREA)
- Details Of Aerials (AREA)
- Aerials With Secondary Devices (AREA)
Description
ηはアンテナ効率
Dはアンテナの直径
およびλは波長
である場合には、アンテナ開口の直径を4倍に増大すると、利得は16倍に、すなわち12dB増加する。より大きな開口によって、人工衛星上の送信機電力の16分の1で同等の通信サービスが提供され、それによって熱、サイズ、質量、主要電力、および費用が軽減される。あるいは、同じ送信機電力は、同等のビット誤り率性能でのデータ転送速度の16倍を維持できる。より大きなアンテナ開口はまた、地上局のアップリンク電力を16分の1に削減して、熱およびバッテリのサイズを軽減することを可能にするか、または地上局アンテナのサイズを軽減することを可能にし、移動性を向上させ移動中の通信を実現する。したがって、より大きなアンテナ開口は人工衛星通信システムに利点をもたらす。
Claims (22)
- 第1の構成から第2の構成に拡張するように構成された構造と、
前記構造の周囲に取り付けられた、少なくとも2つの機器室とを備え、
前記構造が、アンテナ反射器メッシュ、遮光メッシュ、光反射器メッシュ、およびネットの少なくとも1つを備え、
前記第1の構成で、前記少なくとも2つの機器室のそれぞれが、ボルト連結構造によって、当該少なくとも2つの機器室の他の機器室に縁部で物理的に連結され、
前記ボルト連結構造が爆発して、前記少なくとも2つの機器室のそれぞれが互いに隔離するように構成された、宇宙船。 - 請求項1記載の宇宙船において、
前記少なくとも2つの機器室の少なくとも1つが、アンテナ給電装置を備える、宇宙船。 - 請求項1記載の宇宙船において、
前記少なくとも2つの機器室の少なくとも1つが、太陽電池パネルを備える、宇宙船。 - 請求項1記載の宇宙船において、
前記少なくとも2つの機器室の少なくとも1つが、送受信機を備える、宇宙船。 - 請求項1記載の宇宙船において、
前記少なくとも2つの機器室の少なくとも1つが、推進システムを備える、宇宙船。 - 請求項5記載の宇宙船において、
前記少なくとも2つの機器室の少なくとも1つが、前記推進システムに電力を供給するための燃料タンクを備える、宇宙船。 - 請求項1記載の宇宙船において、
前記少なくとも2つの機器室の少なくとも1つが、姿勢制御システムを備える、宇宙船。 - 請求項1記載の宇宙船において、
前記少なくとも2つの機器室と連結するケーブルをさらに備える、宇宙船。 - 請求項8記載の宇宙船において、
前記少なくとも2つの機器室が、ケーブルを介して電力を共有する、宇宙船。 - 請求項8記載の宇宙船において、
前記少なくとも2つの機器室が、前記ケーブルを介して通信する、宇宙船。 - 請求項1記載の宇宙船において、
前記少なくとも2つの機器室が、ワイヤレスで通信する、宇宙船。 - 請求項1記載の宇宙船において、
人工衛星である、宇宙船。 - 第1の構成から第2の構成へ拡張するように構成されたアンテナ構造と、
前記アンテナ構造の周囲に取り付けられた少なくとも2つの機器室とを備え、
前記少なくとも2つの機器室のそれぞれが、太陽電池パネルおよび推進システムを備え、
前記少なくとも2つの機器室の少なくとも1つがアンテナ給電装置を備え、
前記第1の構成で、前記少なくとも2つの機器室のそれぞれが、当該少なくとも2つの機器室の他の機器室に接触し、
前記少なくとも2つの機器室のそれぞれは、ボルト連結構造によって、前記他の機器室に縁部で物理的に連結され、
前記ボルト連結構造が爆発して、前記少なくとも2つの機器室のそれぞれが互いに隔離するように構成された、宇宙船。 - 請求項13記載の宇宙船において、
前記少なくとも2つの機器室の少なくとも1つが、送受信機を備える、宇宙船。 - 請求項13記載の宇宙船において、
前記少なくとも2つの機器室のそれぞれが、前記推進システムを駆動するための燃料タンクを備える、宇宙船。 - 請求項13記載の宇宙船において、
前記少なくとも2つの機器室の少なくとも1つが、姿勢制御システムを備える、宇宙船。 - 請求項13記載の宇宙船において、
前記少なくとも2つの機器室に接続するケーブルをさらに備える、宇宙船。 - 請求項17記載の宇宙船において、
前記少なくとも2つの機器室がケーブルを介して電力を共有し、前記ケーブルを介して通信する、宇宙船。 - 請求項13記載の宇宙船において、
人工衛星である、宇宙船。 - 第1の構成から第2の構成へ拡張するように構成されたペイロード要素と、
前記ペイロード要素の周囲に取り付けられた少なくとも2つの宇宙船支持構造とを備え、
前記少なくとも2つの宇宙船支持構造の少なくとも1つが、推進システムと、追跡、遠隔測定および制御システムとを備え、
前記第1の構成で、前記少なくとも2つの宇宙船支持構造のそれぞれが、ボルト連結構造によって、当該少なくとも2つの宇宙船支持構造の他の宇宙船支持構造に縁部で物理的に連結され、
前記ボルト連結構造が爆発して、前記少なくとも2つの宇宙船支持構造のそれぞれが互いに隔離するように構成された、宇宙船。 - 請求項20記載の宇宙船において、
前記ペイロード要素がアンテナ開口構造を備える、宇宙船。 - 請求項20記載の宇宙船において、
前記宇宙船が人工衛星である、宇宙船。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/845,825 US7686255B2 (en) | 2007-08-28 | 2007-08-28 | Space vehicle having a payload-centric configuration |
US11/845,825 | 2007-08-28 | ||
PCT/US2008/072046 WO2009048678A2 (en) | 2007-08-28 | 2008-08-04 | A space vehicle having a payload-centric configuration |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2010537880A JP2010537880A (ja) | 2010-12-09 |
JP5372934B2 true JP5372934B2 (ja) | 2013-12-18 |
Family
ID=40405873
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2010523014A Active JP5372934B2 (ja) | 2007-08-28 | 2008-08-04 | ペイロード中心構成を有する宇宙船 |
Country Status (6)
Country | Link |
---|---|
US (1) | US7686255B2 (ja) |
EP (1) | EP2193570B1 (ja) |
JP (1) | JP5372934B2 (ja) |
AU (1) | AU2008311240A1 (ja) |
CA (1) | CA2694328C (ja) |
WO (1) | WO2009048678A2 (ja) |
Families Citing this family (40)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20100156339A1 (en) * | 2008-12-18 | 2010-06-24 | Hoffman Roger L | Portable solar battery charger |
EP2643882B1 (en) | 2010-12-15 | 2014-04-16 | Skybox Imaging, Inc. | Integrated antenna system for imaging microsatellites |
US8800935B2 (en) * | 2011-03-09 | 2014-08-12 | Space Systems/Loral, Llc | Spacecraft payload positioning with respect to a virtual pivot point |
US8474760B2 (en) | 2011-03-16 | 2013-07-02 | Stephen Leventhal | Polygonal support structure |
US8979034B2 (en) | 2011-12-06 | 2015-03-17 | Altius Space Machines | Sticky boom non-cooperative capture device |
US8967548B2 (en) * | 2011-12-06 | 2015-03-03 | Altius Space Machines | Direct to facility capture and release |
EP2825827B1 (en) * | 2012-03-15 | 2017-05-17 | European Space Agency | Mechanical support ring structure |
US9815574B2 (en) * | 2012-03-19 | 2017-11-14 | Agence Spatiale Europeenne | Deployable tensegrity structure, especially for space applications |
US9180984B2 (en) | 2012-05-11 | 2015-11-10 | The Boeing Company | Methods and apparatus for performing propulsion operations using electric propulsion systems |
US8915472B2 (en) * | 2012-05-11 | 2014-12-23 | The Boeing Company | Multiple space vehicle launch system |
FR2991300B1 (fr) * | 2012-06-05 | 2014-07-11 | Snecma | Engin spatial equipe d'un dispositif de desorbitation comprenant un moteur a detonation |
WO2014053163A1 (en) * | 2012-10-01 | 2014-04-10 | European Space Agency | Deployable antenna frame |
CA2831309C (en) * | 2012-12-04 | 2017-05-30 | The Boeing Company | Methods and apparatus for performing propulsion operations using electric propulsion systems |
US9669948B2 (en) | 2013-07-24 | 2017-06-06 | Lockheed Martin Corporation | Side-by-side dual-launch arrangement with improved payload compatibility |
US9475591B2 (en) * | 2013-11-19 | 2016-10-25 | Arthur Mckee Dula | Space launch apparatus |
US9755318B2 (en) | 2014-01-09 | 2017-09-05 | Northrop Grumman Systems Corporation | Mesh reflector with truss structure |
US9484636B2 (en) * | 2014-02-26 | 2016-11-01 | Northrop Grumman Systesms Corportion | Mesh reflector with truss structure |
US9856039B2 (en) * | 2014-10-08 | 2018-01-02 | Analytical Mechanics Associates, Inc. | Extendable solar array for a spacecraft system |
US9991944B2 (en) * | 2015-01-15 | 2018-06-05 | Hughes Network Systems, Llc | High altitude platform with multibeam coverage for aero-based terminals |
US10189583B2 (en) * | 2015-05-13 | 2019-01-29 | Analytical Mechanics Associates, Inc. | Deployable sheet material systems and methods |
CN104900978B (zh) * | 2015-05-13 | 2018-01-12 | 上海宇航***工程研究所 | 一种周边式空间网状等底展收机构 |
CN105071012B (zh) * | 2015-07-27 | 2018-03-16 | 哈尔滨工业大学 | 空间可展开环形张拉整体天线机构 |
CN105071013A (zh) * | 2015-08-25 | 2015-11-18 | 西北工业大学 | 一种卫星天线环形阵列可展单元结构 |
FR3041939B1 (fr) * | 2015-10-02 | 2017-10-20 | Airbus Defence & Space Sas | Satellite comprenant un instrument optique de prise de vue |
US9621255B1 (en) | 2015-11-12 | 2017-04-11 | Space Systems/Loral, Llc | Channelizer supplemented spacecraft telemetry and command functionality |
CN105510881B (zh) * | 2015-11-20 | 2018-02-06 | 西安电子科技大学 | 一种静电成形薄膜天线径向索长度调整装置及调整方法 |
US10957987B2 (en) * | 2016-07-14 | 2021-03-23 | Harris Corporation | Space deployable inflatable antenna apparatus and associated methods |
US10306984B2 (en) * | 2016-08-30 | 2019-06-04 | The Boeing Company | Toroidal support structures |
US10516216B2 (en) | 2018-01-12 | 2019-12-24 | Eagle Technology, Llc | Deployable reflector antenna system |
CN108945519A (zh) * | 2018-05-30 | 2018-12-07 | 北京空间飞行器总体设计部 | 一种基于周边桁架式天线的一体化可展开卫星 |
US10707552B2 (en) | 2018-08-21 | 2020-07-07 | Eagle Technology, Llc | Folded rib truss structure for reflector antenna with zero over stretch |
US10811759B2 (en) | 2018-11-13 | 2020-10-20 | Eagle Technology, Llc | Mesh antenna reflector with deployable perimeter |
US11139549B2 (en) | 2019-01-16 | 2021-10-05 | Eagle Technology, Llc | Compact storable extendible member reflector |
US11942687B2 (en) | 2019-02-25 | 2024-03-26 | Eagle Technology, Llc | Deployable reflectors |
JP6860224B2 (ja) * | 2019-03-04 | 2021-04-14 | 株式会社不二宮製作所 | 伸縮アーム |
US10797400B1 (en) | 2019-03-14 | 2020-10-06 | Eagle Technology, Llc | High compaction ratio reflector antenna with offset optics |
CN114503361B (zh) * | 2019-09-24 | 2024-06-04 | 空中客车防务及航天股份有限公司 | 天线可展开组件 |
CN112103615B (zh) * | 2020-09-16 | 2022-12-23 | 深圳市威富通讯技术有限公司 | 天线自动收展调平装置和天线调平方法 |
US12017803B2 (en) | 2021-07-28 | 2024-06-25 | Rensselaer Polytechnic Institute | System and method for debris capture |
US20230174252A1 (en) * | 2021-12-07 | 2023-06-08 | John Jeffrey Blincow | Rapid Sequential Circular Assembly System for Space Station |
Family Cites Families (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3174397A (en) * | 1962-09-10 | 1965-03-23 | Rayan Aeronautical Co | Deployment mechanism for satellite mirror structure |
US3496687A (en) * | 1967-03-22 | 1970-02-24 | North American Rockwell | Extensible structure |
FR2476018A1 (fr) * | 1980-02-14 | 1981-08-21 | Org Europeene De Rech | Configuration de satellites pour mission geostationnaire |
US4375878A (en) * | 1980-10-28 | 1983-03-08 | Lockheed Missiles & Space Company, Inc. | Space satellite with agile payload orientation system |
JPS5967739A (ja) * | 1982-10-12 | 1984-04-17 | Nec Corp | 宇宙での組立式三軸姿勢制御型通信衛星 |
JPS6397498A (ja) * | 1986-10-09 | 1988-04-28 | 三菱電機株式会社 | 人工重力宇宙船 |
JPS63297197A (ja) * | 1987-05-28 | 1988-12-05 | 日本電気株式会社 | 人工衛星 |
JPS6490898A (en) * | 1987-09-30 | 1989-04-07 | Nec Corp | Built-up type panel artificial satellite |
FR2667299B1 (fr) | 1990-10-02 | 1994-01-14 | Aerospatiale Ste Nationale Indle | Satellite de type geostationnaire a systeme de manóoeuvre d'apogee a ergols liquides et a antennes creuses. |
US5642122A (en) * | 1991-11-08 | 1997-06-24 | Teledesic Corporation | Spacecraft antennas and beam steering methods for satellite communciation system |
JPH05213283A (ja) * | 1992-02-04 | 1993-08-24 | Nec Corp | 人工衛星の構造 |
US5314146A (en) * | 1992-03-13 | 1994-05-24 | Spectrum Astro, Inc. | Multi-mission spacecraft bus having space frame structural design |
US5680145A (en) * | 1994-03-16 | 1997-10-21 | Astro Aerospace Corporation | Light-weight reflector for concentrating radiation |
US5806800A (en) | 1995-12-22 | 1998-09-15 | Caplin; Glenn N. | Dual function deployable radiator cover |
US5864324A (en) * | 1996-05-15 | 1999-01-26 | Trw Inc. | Telescoping deployable antenna reflector and method of deployment |
US5848767A (en) | 1996-08-05 | 1998-12-15 | The Boeing Company | One piece spacecraft frame |
JPH11208596A (ja) * | 1998-01-23 | 1999-08-03 | Mitsubishi Electric Corp | 衛星構体 |
US6028570A (en) * | 1998-05-18 | 2000-02-22 | Trw Inc. | Folding perimeter truss reflector |
US6150995A (en) * | 1998-09-04 | 2000-11-21 | Trw Inc. | Combined photovoltaic array and RF reflector |
JP2000272599A (ja) * | 1999-03-23 | 2000-10-03 | Toshiba Corp | 宇宙航行体重心制御装置 |
US6225965B1 (en) * | 1999-06-18 | 2001-05-01 | Trw Inc. | Compact mesh stowage for deployable reflectors |
US7020076B1 (en) * | 1999-10-26 | 2006-03-28 | California Institute Of Technology | Fault-tolerant communication channel structures |
US6323827B1 (en) * | 2000-01-07 | 2001-11-27 | Trw Inc. | Micro fold reflector |
US6836255B1 (en) | 2000-01-21 | 2004-12-28 | Northrop Grumman Corporation | Limited field of view antenna for space borne applications |
JP2006080577A (ja) * | 2003-09-10 | 2006-03-23 | Nippon Telegr & Teleph Corp <Ntt> | 展開アンテナ |
US6978966B2 (en) * | 2004-02-02 | 2005-12-27 | The Boeing Company | Reflector deployment error estimation |
US7337097B2 (en) * | 2004-03-18 | 2008-02-26 | The Boeing Company | Dynamic modeling technique for the deployment of large satellite antennas |
JP2006007879A (ja) * | 2004-06-23 | 2006-01-12 | National Institute Of Advanced Industrial & Technology | 宇宙漂流物体の回収方法及び回収装置 |
JP2006229750A (ja) * | 2005-02-18 | 2006-08-31 | Mitsubishi Electric Corp | 宇宙用展開型アンテナ |
-
2007
- 2007-08-28 US US11/845,825 patent/US7686255B2/en active Active
-
2008
- 2008-08-04 AU AU2008311240A patent/AU2008311240A1/en not_active Abandoned
- 2008-08-04 CA CA2694328A patent/CA2694328C/en active Active
- 2008-08-04 JP JP2010523014A patent/JP5372934B2/ja active Active
- 2008-08-04 WO PCT/US2008/072046 patent/WO2009048678A2/en active Application Filing
- 2008-08-04 EP EP08836904.6A patent/EP2193570B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
AU2008311240A1 (en) | 2009-04-16 |
WO2009048678A3 (en) | 2009-05-28 |
AU2008311240A2 (en) | 2010-04-08 |
US20090057492A1 (en) | 2009-03-05 |
JP2010537880A (ja) | 2010-12-09 |
CA2694328A1 (en) | 2009-04-16 |
US7686255B2 (en) | 2010-03-30 |
WO2009048678A2 (en) | 2009-04-16 |
EP2193570A2 (en) | 2010-06-09 |
EP2193570B1 (en) | 2018-12-19 |
CA2694328C (en) | 2015-07-21 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP5372934B2 (ja) | ペイロード中心構成を有する宇宙船 | |
EP3289313B1 (en) | System and method for assembling and deploying satellites | |
US9758260B2 (en) | Low volume micro satellite with flexible winded panels expandable after launch | |
US5927654A (en) | Spacecraft with active antenna array protected against temperature extremes | |
US10680310B2 (en) | Balloon reflector antenna | |
KR100971096B1 (ko) | 경량의 공간-피딩된 능동 위상 어레이 안테나 시스템 | |
US9966658B2 (en) | Antennas for small satellites | |
US5386953A (en) | Spacecraft designs for satellite communication system | |
EP3762297B1 (en) | Deployable spacecraft body | |
CN104890900A (zh) | 用于展开一组面板的方法和设备 | |
US7138960B2 (en) | Deployable electromagnetic concentrator | |
GB2455311A (en) | Deployable panel structure | |
WO2016079945A1 (ja) | レーダ衛星およびこれを用いたレーダ衛星システム | |
Fujiwara et al. | Optical inter-orbit communications engineering test satellite (OICETS) | |
JP2008221876A (ja) | 人工衛星搭載用太陽電池パネル、及び人工衛星 | |
US20230321903A1 (en) | 3d printed spacecraft structures | |
CN114662273A (zh) | 一种微纳卫星sar天线总体设计方法 | |
EP0838877A2 (en) | Deployable reflectors | |
You et al. | Design Case of Typical Spacecraft Antenna System | |
Laurin et al. | NORSAT-2: Enabling Advanced Maritime Communication with VDES | |
Mehradnia et al. | NorSat-1: Enabling High Performance and Multipurpose Microsatellite Missions | |
JPS5967739A (ja) | 宇宙での組立式三軸姿勢制御型通信衛星 | |
Eichelberger et al. | Antenna design for a Direct-to-Earth link of a planetary deep space probe |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20110607 |
|
A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20121016 |
|
A601 | Written request for extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A601 Effective date: 20130110 |
|
A602 | Written permission of extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A602 Effective date: 20130118 |
|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20130415 |
|
TRDD | Decision of grant or rejection written | ||
A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20130820 |
|
A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20130918 |
|
R150 | Certificate of patent or registration of utility model |
Ref document number: 5372934 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |