ES2136397T3 - Dispositivo para la orientacion de un panel solar de aparato espacial y aparato asi equipado. - Google Patents

Dispositivo para la orientacion de un panel solar de aparato espacial y aparato asi equipado.

Info

Publication number
ES2136397T3
ES2136397T3 ES96909205T ES96909205T ES2136397T3 ES 2136397 T3 ES2136397 T3 ES 2136397T3 ES 96909205 T ES96909205 T ES 96909205T ES 96909205 T ES96909205 T ES 96909205T ES 2136397 T3 ES2136397 T3 ES 2136397T3
Authority
ES
Spain
Prior art keywords
ship
orientation
panel
incidence
drag
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 - Lifetime
Application number
ES96909205T
Other languages
English (en)
Inventor
Thibery Cussac
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.)
Centre National dEtudes Spatiales CNES
Original Assignee
Centre National dEtudes Spatiales CNES
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 Centre National dEtudes Spatiales CNES filed Critical Centre National dEtudes Spatiales CNES
Application granted granted Critical
Publication of ES2136397T3 publication Critical patent/ES2136397T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • B64G1/42—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
    • B64G1/222—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
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
    • B64G1/443—Photovoltaic cell 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)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Photovoltaic Devices (AREA)

Abstract

LA INVENCION SE REFIERE A UN DISPOSITIVO (2) PARA LA ORIENTACION DE UN PANEL SOLAR (4) QUE EQUIPA UNA NAVE ESPACIAL, TAL COMO UN SATELITE (1), CONECTADO DE MANERA ARTICULADA AL CUERPO (3) DE DICHA NAVE. ESTE DISPOSITIVO (2) LLEVA UN MECANISMO DE ARRASTRE (6) DESTINADO A ARRASTRAR CON DESPLAZAMIENTO EL PANEL RESPECTO DEL CUERPO DE LA NAVE DE MANERA AUTONOMA EN FUNCION DE LA DIRECCION DE INCIDENCIA DE LOS RAYOS SOLARES. ESTE MECANISMO DE ARRASTRE (6) ESTA DESTINADO A ADOPTAR DOS ESTADOS EN FUNCION DE SU TEMPERATURA Y ESTA DISPUESTO SOBRE LA NAVE PARA QUE EL CAMBIO DE LA DIRECCION DE INCIDENCIA DE LOS RAYOS SOLARES SOBRE LA NAVE VAYA ACOMPAÑADO POR UNA VARIACION DE LA TEMPERATURA DEL MECANISMO DE ARRASTRE, PROVOQUE UN CAMBIO DE ESTADO DE ESTE ULTIMO Y UNA MODIFICACION DE LA ORIENTACION DEL PANEL QUE TIENE A REDUCIR EL ANGULO DE INCIDENCIA DE LOS RAYOS SOLARES SOBRE EL PANEL.
ES96909205T 1995-03-28 1996-03-27 Dispositivo para la orientacion de un panel solar de aparato espacial y aparato asi equipado. Expired - Lifetime ES2136397T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9503610A FR2732309B1 (fr) 1995-03-28 1995-03-28 Dispositif pour l'orientation d'un panneau solaire d'engin spatial et engin ainsi equipe

Publications (1)

Publication Number Publication Date
ES2136397T3 true ES2136397T3 (es) 1999-11-16

Family

ID=9477484

Family Applications (1)

Application Number Title Priority Date Filing Date
ES96909205T Expired - Lifetime ES2136397T3 (es) 1995-03-28 1996-03-27 Dispositivo para la orientacion de un panel solar de aparato espacial y aparato asi equipado.

Country Status (6)

Country Link
US (1) US6062511A (es)
EP (1) EP0817744B1 (es)
DE (1) DE69604165T2 (es)
ES (1) ES2136397T3 (es)
FR (1) FR2732309B1 (es)
WO (1) WO1996030259A1 (es)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6003817A (en) * 1996-11-12 1999-12-21 Motorola, Inc. Actively controlled thermal panel and method therefor
FR2848529B1 (fr) * 2002-12-12 2005-02-25 Astrium Sas Procede de pilotage solaire de vehicule spatial
US7370566B2 (en) * 2003-09-04 2008-05-13 Harris Corporation Complimentary retrograde/prograde satellite constellation
DE102005021459B3 (de) 2005-05-10 2006-07-13 Eads Space Transportation Gmbh Mechanischer Rotationsantrieb
CN108945521B (zh) * 2018-06-15 2020-11-13 上海卫星工程研究所 一种无源空间环境航天器自适应变形机构
US20220073217A1 (en) * 2020-09-10 2022-03-10 Brigham Young University (Byu) Dynamic radiative thermal management of spacecraft

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3304028A (en) * 1964-08-11 1967-02-14 Hugh L Dryden Attitude control for spacecraft
US3311322A (en) * 1964-09-17 1967-03-28 Boeing Co Servomechanisms responsive to a heat source
US3635015A (en) * 1967-12-21 1972-01-18 Trw Inc Radiant-energy-driven orientation system
US3630020A (en) * 1968-04-18 1971-12-28 Boeing Co Solar orientation device
FR2371343A1 (fr) * 1976-11-17 1978-06-16 Aerospatiale Dispositif pour le deploiement synchronise d'elements articules porteurs de cellules solaires dans un panneau forme d'une succession de tels elements
US4091799A (en) * 1977-03-10 1978-05-30 Emerson Electric Co. Self-tracking radiant energy collector
US4561614A (en) * 1982-12-07 1985-12-31 Rca Corporation Deployable folded multi-element satellite subsystems
US4842106A (en) * 1987-10-08 1989-06-27 Hughes Aircraft Company Rate controllable damping mechanism
JPH01237296A (ja) * 1988-03-18 1989-09-21 Mitsubishi Electric Corp 太陽電地パドル装置
US5257759A (en) * 1991-11-27 1993-11-02 Hughes Aircraft Company Method and apparatus for controlling a solar wing of a satellite using a sun sensor
US5310144A (en) * 1992-07-06 1994-05-10 Hughes Aircraft Company Method and apparatus for satellite torque balancing

Also Published As

Publication number Publication date
DE69604165T2 (de) 2000-02-10
EP0817744A1 (fr) 1998-01-14
EP0817744B1 (fr) 1999-09-08
WO1996030259A1 (fr) 1996-10-03
DE69604165D1 (de) 1999-10-14
FR2732309A1 (fr) 1996-10-04
US6062511A (en) 2000-05-16
FR2732309B1 (fr) 1997-06-20

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