GB1268841A - An extensible arm assembly for a spacecraft or a satellite - Google Patents

An extensible arm assembly for a spacecraft or a satellite

Info

Publication number
GB1268841A
GB1268841A GB32652/69A GB3265269A GB1268841A GB 1268841 A GB1268841 A GB 1268841A GB 32652/69 A GB32652/69 A GB 32652/69A GB 3265269 A GB3265269 A GB 3265269A GB 1268841 A GB1268841 A GB 1268841A
Authority
GB
United Kingdom
Prior art keywords
tubes
spacecraft
arms
main
arm
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.)
Expired
Application number
GB32652/69A
Other languages
English (en)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB1268841A publication Critical patent/GB1268841A/en
Expired legal-status Critical Current

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
    • B64G1/222—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
    • B64G1/2227—Inflating
    • 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
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S136/00—Batteries: thermoelectric and photoelectric
    • Y10S136/291—Applications
    • Y10S136/292—Space - satellite

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tents Or Canopies (AREA)
  • Aerials With Secondary Devices (AREA)
  • Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
GB32652/69A 1968-10-08 1969-06-27 An extensible arm assembly for a spacecraft or a satellite Expired GB1268841A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19681801777 DE1801777B2 (de) 1968-10-08 1968-10-08 Ausleger zur aufnahme von sonnenzellen

Publications (1)

Publication Number Publication Date
GB1268841A true GB1268841A (en) 1972-03-29

Family

ID=5709925

Family Applications (1)

Application Number Title Priority Date Filing Date
GB32652/69A Expired GB1268841A (en) 1968-10-08 1969-06-27 An extensible arm assembly for a spacecraft or a satellite

Country Status (5)

Country Link
US (1) US3606211A (de)
JP (1) JPS4750475B1 (de)
DE (1) DE1801777B2 (de)
FR (1) FR2020089B1 (de)
GB (1) GB1268841A (de)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6016999A (en) * 1997-07-05 2000-01-25 Matra Marconi Space Uk Limited Spacecraft platforms
WO2014024199A1 (en) 2012-08-08 2014-02-13 Halsband Arie Low volume micro satellite with flexible winded panels expandable after launch
CN104743140A (zh) * 2015-03-28 2015-07-01 哈尔滨工业大学 一种抓握式充气抓捕手
WO2015097698A1 (en) * 2013-12-26 2015-07-02 Israel Aerospace Industries Ltd. Space vehicle

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2081107A1 (de) * 1970-03-05 1971-12-03 Nal Etu Spatiales Centre
CH651705A5 (de) * 1980-02-11 1985-09-30 Micafil Ag Wickelvorrichtung zum bewickeln von mit wickelkopfabstuetzungen versehenen statoren elektrischer maschinen.
US4787580A (en) * 1985-06-27 1988-11-29 General Electric Company Large solar arrays with high natural frequencies
JP3805706B2 (ja) * 2002-03-15 2006-08-09 三菱電機株式会社 人工衛星展開構造物
FR2853624B1 (fr) * 2003-04-14 2005-06-10 Eads Launch Vehicles Ensemble d'elements, pliable et deployable, monte a bord d'un engin spatial
DE10334352A1 (de) * 2003-07-25 2005-02-24 Eads Astrium Gmbh Solargenerator zur Entfaltung in zwei Raumrichtungen
FR2902764B1 (fr) * 2006-06-27 2009-09-25 Alcatel Sa Structure deployable comportant des elements rigides, embarquee sur un engin spatial
JP5080222B2 (ja) * 2007-11-30 2012-11-21 古河ユニック株式会社 車両搭載用の道路交通規制標識表示装置
FR2972713B1 (fr) * 2011-03-17 2013-03-22 Thales Sa Structure plane escamotable, et satellite comprenant une telle structure
FR3014848B1 (fr) * 2013-12-18 2017-09-08 Thales Sa Dispositif antichoc pour structure depliable
WO2016172647A1 (en) 2015-04-22 2016-10-27 Sercel Joel C Optics and structure for space applications
US11143026B2 (en) 2018-08-07 2021-10-12 Trans Astronautica Corporation Systems and methods for radiant gas dynamic mining of permafrost for propellant extraction
US11391246B2 (en) 2020-04-27 2022-07-19 Trans Astronautica Corporation Omnivorous solar thermal thruster, cooling systems, and thermal energy transfer in rockets
US11566521B2 (en) 2020-09-22 2023-01-31 Trans Astronautica Corporation Systems and methods for radiant gas dynamic mining of permafrost
US11702857B2 (en) * 2021-02-26 2023-07-18 Trans Astronautica Corporation Pneumatically supported towers for low gravity applications
US11748897B1 (en) 2022-06-24 2023-09-05 Trans Astronautica Corporation Optimized matched filter tracking of space objects
CN118004451B (zh) * 2024-04-02 2024-06-04 北京航空航天大学 一种基于盘绕式伸展臂二次展开的多太阳翼同步展开装置

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6016999A (en) * 1997-07-05 2000-01-25 Matra Marconi Space Uk Limited Spacecraft platforms
WO2014024199A1 (en) 2012-08-08 2014-02-13 Halsband Arie Low volume micro satellite with flexible winded panels expandable after launch
EP2882649A4 (de) * 2012-08-08 2016-04-20 Arie Halsband Kleinvolumiger mikrosatellit mit flexiblen gewickelten, nach dem abschuss expandierbaren platten
US9758260B2 (en) 2012-08-08 2017-09-12 Effective Space Solutions R&D Ltd Low volume micro satellite with flexible winded panels expandable after launch
WO2015097698A1 (en) * 2013-12-26 2015-07-02 Israel Aerospace Industries Ltd. Space vehicle
CN104743140A (zh) * 2015-03-28 2015-07-01 哈尔滨工业大学 一种抓握式充气抓捕手
CN104743140B (zh) * 2015-03-28 2016-08-24 哈尔滨工业大学 一种抓握式充气抓捕手

Also Published As

Publication number Publication date
FR2020089B1 (de) 1974-05-24
JPS4750475B1 (de) 1972-12-18
FR2020089A1 (de) 1970-07-10
US3606211A (en) 1971-09-20
DE1801777A1 (de) 1970-05-21
DE1801777B2 (de) 1971-12-30

Similar Documents

Publication Publication Date Title
GB1268841A (en) An extensible arm assembly for a spacecraft or a satellite
US3532299A (en) Deployable solar array
US3677508A (en) Folding deployable panel structure having roll-up retaining spring for stowage
GB1176184A (en) Extensible Outrigger for a Spacecraft
US8616502B1 (en) Deployable solar panel assembly for spacecraft
US4988060A (en) Solar collector panel arrangement with partly and fully foldable panels
US3576566A (en) Closed loop antenna reflector supporting structure
ES2624262T3 (es) Estructura desplegable retráctil con cinta métrica
US3241142A (en) Gravity stabilized satellite
US3809337A (en) Spin stabilized vehicle and solar cell arrangement therefor
US3283328A (en) Sounding balloon and target assembly
US20020134423A1 (en) Membrane-based solar array structures for spacecraft
JP2647040B2 (ja) サンシールド
JPH0145762B2 (de)
CN104601100A (zh) 一种光伏组件的支撑机构
US1289130A (en) Portable mirror.
GB921765A (en) Improvements relating to tarpaulin and like cover supports for road vehicles
Pérez-Valcárcel et al. Expandable structures with incorporated roofing elements.
JPH0524594A (ja) スピン安定型人工衛星
Morozov Stability of the relative equilibrium of a satellite under the action of gravitational, magnetic, and aerodynamic moments(Gyrostat satellite equilibrium positions in circular equatorial orbit under action of gravitational magnetic and aerodynamic moments based on gyrostabilized satellite equations of motion)
CN111874455A (zh) 柔性太阳能组件的运输方式
SU145130A1 (ru) Передвижна широкоэкранна киноустановка
Sheppard Cheaper access
Covault HST emergency mission set
FADDOUL et al. Rigid open cell polyurethane foam as a cryogenic multi-layer insulation component(Long term cryogenic propellant storage in space, considering rigid open cell polyurethane foam as spacer in multilayer insulation system)