DE3045421C2 - Vorrichtung zum Ausklappen der Elemente eines Ausfahrarms einer Ausrüstung für ein Raumfahrzeug - Google Patents

Vorrichtung zum Ausklappen der Elemente eines Ausfahrarms einer Ausrüstung für ein Raumfahrzeug

Info

Publication number
DE3045421C2
DE3045421C2 DE3045421A DE3045421A DE3045421C2 DE 3045421 C2 DE3045421 C2 DE 3045421C2 DE 3045421 A DE3045421 A DE 3045421A DE 3045421 A DE3045421 A DE 3045421A DE 3045421 C2 DE3045421 C2 DE 3045421C2
Authority
DE
Germany
Prior art keywords
elements
equipment
devices
spacecraft
unlocking
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
DE3045421A
Other languages
German (de)
English (en)
Other versions
DE3045421A1 (de
Inventor
Georges Marello
Jean-Claude Mandelieu Vermalle
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 Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Publication of DE3045421A1 publication Critical patent/DE3045421A1/de
Application granted granted Critical
Publication of DE3045421C2 publication Critical patent/DE3045421C2/de
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
    • B64G1/2228—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 hold-down or release mechanisms
    • 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
    • B64G1/2229—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 deployment actuating mechanism
    • 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
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/407—Solar sailing
    • 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
    • B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerials With Secondary Devices (AREA)
DE3045421A 1979-12-03 1980-12-02 Vorrichtung zum Ausklappen der Elemente eines Ausfahrarms einer Ausrüstung für ein Raumfahrzeug Expired DE3045421C2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7929681A FR2470727A1 (fr) 1979-12-03 1979-12-03 Dispositif de deploiement des elements d'un bras d'eloignement d'un equipement pour engin spatial

Publications (2)

Publication Number Publication Date
DE3045421A1 DE3045421A1 (de) 1981-08-27
DE3045421C2 true DE3045421C2 (de) 1986-11-27

Family

ID=9232338

Family Applications (1)

Application Number Title Priority Date Filing Date
DE3045421A Expired DE3045421C2 (de) 1979-12-03 1980-12-02 Vorrichtung zum Ausklappen der Elemente eines Ausfahrarms einer Ausrüstung für ein Raumfahrzeug

Country Status (2)

Country Link
DE (1) DE3045421C2 (enExample)
FR (1) FR2470727A1 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT512487A1 (de) * 2012-01-25 2013-08-15 Ruag Space Gmbh Stellmechanismus

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2531032A1 (fr) * 1982-07-30 1984-02-03 Aerospatiale Dispositif de derivation d'effort temporaire pour maintien en position de stockage d'un appendice deployable pour vehicule spatial
US4747567A (en) * 1985-03-20 1988-05-31 Space Industries, Inc. Spacecraft with articulated solar array
FR2662149B1 (fr) * 1990-05-18 1992-09-04 Aerospatiale Bobine a cable captif et son application a un regulateur de deploiement d'un appendice d'engin spatial.
RU2321087C1 (ru) * 2006-06-13 2008-03-27 Федеральное государственное унитарное предприятие "Красная звезда" Космическая ядерная энергетическая установка

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3631737A (en) * 1970-09-18 1972-01-04 Nasa Remote control manipulator for zero gravity environment
US3817477A (en) * 1971-07-06 1974-06-18 Trw Inc Deployable annular solar array
US3948468A (en) * 1971-09-27 1976-04-06 Rca Corporation Replaceable solar array panels
US3817481A (en) * 1971-11-17 1974-06-18 Trw Inc Deployable solar array for a spin stabilized spacecraft
GB1473720A (en) * 1974-09-28 1977-05-18 British Aircraft Corp Ltd Coupling assemblies
US4133501A (en) * 1975-09-30 1979-01-09 Communications Satellite Corporation Self-deployable solar cell panel
US4133502A (en) * 1977-03-28 1979-01-09 Rca Corporation Plural panels deployed effectively as a single panel

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT512487A1 (de) * 2012-01-25 2013-08-15 Ruag Space Gmbh Stellmechanismus
AT512487B1 (de) * 2012-01-25 2016-05-15 Ruag Space Gmbh Stellmechanismus

Also Published As

Publication number Publication date
FR2470727A1 (fr) 1981-06-12
FR2470727B1 (enExample) 1983-04-22
DE3045421A1 (de) 1981-08-27

Similar Documents

Publication Publication Date Title
DE2727101C3 (de) Vorrichtung zum synchronen Verschwenken von Paneelen für insbesondere Solarzellen
DE3872181T2 (de) Vorrichtung zum ausspreizen der leitfluegel eines geschosses.
DE2110626C3 (de) Ausbreitbarer Sonnenzellenträger für Raumfahrzeuge
DE3316789C2 (enExample)
DE3329955C2 (enExample)
DE2342783C2 (de) Mit einem Leitwerk versehenes Geschoß
DE102011114473B3 (de) Gelenk zum Entfalten und Verriegeln eines Solargenerators oder eines Reflektors
DE69206704T2 (de) Sonnensegel
DE1801777A1 (de) Ausleger zur Aufnahme von Sonnenzellen
DE2331607A1 (de) Vorrichtung zur halterung einer ladung
DE3215434C2 (de) Riegelmechanismus für entfaltbare Solargeneratoren von Satelliten
DE3045421C2 (de) Vorrichtung zum Ausklappen der Elemente eines Ausfahrarms einer Ausrüstung für ein Raumfahrzeug
DE3234267C2 (de) Ausfahrbare Strebenanordnung für einen sich selbst aufrichtenden Flügel
DE3215431C2 (de) Einrichtung zum Entfalten von Solargeneratoren
EP1052087A2 (de) Vorrichtung und Verfahren Aufrichten und/oder Zusammenfalten einer Faltbox
EP0469269B1 (de) Aus- und einfahrbares Turmbauwerk
DE102017125460A1 (de) Vorrichtung zum bedarfsweisen Bereitstellen von Sauerstoffmasken
DE69414086T2 (de) Rakete
DE1932423C3 (de) Umklappbare Absperrvorrichtung, insbesondere für Parkplätze
WO2022038016A1 (de) Klapproller mit klappgelenk
DE3128978C2 (de) Faltbarer, rotationssymmetrischer Strahlungsreflektor
DE4336044C2 (de) Gelenkvorrichtung zur Verbindung der Einzelelemente einer Faltstruktur
DE2913449C3 (de) Niederhaltespannvorrichtung für Solargeneratoren von Raumflugkörpern
DE2704354B2 (de) Vorrichtung zur Speicherung und steuerbaren Abgabe von Energie
DE2518506C3 (de) Selbsttätig entfaltbare bzw. zusammenfaltbare Einrichtung zur Halterung von Hydrophonstäben

Legal Events

Date Code Title Description
8110 Request for examination paragraph 44
D2 Grant after examination
8363 Opposition against the patent
8365 Fully valid after opposition proceedings
8339 Ceased/non-payment of the annual fee