EP2190059A1 - Kompakte und robuste Antenne mit langer Brennweite, zur Prüfung auf der Prüfbank und Einbau in einem Satellit - Google Patents

Kompakte und robuste Antenne mit langer Brennweite, zur Prüfung auf der Prüfbank und Einbau in einem Satellit Download PDF

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Publication number
EP2190059A1
EP2190059A1 EP09173375A EP09173375A EP2190059A1 EP 2190059 A1 EP2190059 A1 EP 2190059A1 EP 09173375 A EP09173375 A EP 09173375A EP 09173375 A EP09173375 A EP 09173375A EP 2190059 A1 EP2190059 A1 EP 2190059A1
Authority
EP
European Patent Office
Prior art keywords
reflector
antenna
long
arm
articulation
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.)
Granted
Application number
EP09173375A
Other languages
English (en)
French (fr)
Other versions
EP2190059B1 (de
Inventor
Emmanuel Texier
Eric Boban
Stéphane Ramin
Thierry Longo
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.)
Thales SA
Original Assignee
Thales SA
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 Thales SA filed Critical Thales SA
Publication of EP2190059A1 publication Critical patent/EP2190059A1/de
Application granted granted Critical
Publication of EP2190059B1 publication Critical patent/EP2190059B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/12—Supports; Mounting means
    • H01Q1/1235—Collapsible supports; Means for erecting a rigid antenna
    • 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

Definitions

  • the present invention relates to a long-throw antenna, compact, robust and testable on the ground, mounted on satellite, and by way of non-limiting example, on satellites whose height is less than the focal length of the antenna.
  • antennas of the "simple offset" type with a large diameter reflector require a significant focal length (greater than or equal to 1.5 times the diameter of the reflector) to avoid cross-polarization problems.
  • a focal length greater than or equal to 1.5 times the diameter of the reflector
  • the present invention relates to a long-throw antenna, compact, robust and testable on the ground, mounted on satellite, and by way of non-limiting example, on satellites whose height is less than the focal length of the antenna, this antenna to be lighter, more robust and less expensive than existing solutions, easily testable and not annoying other satellite equipment carrier, either in the stored position or in the deployed position of the antenna.
  • the antenna according to the invention is characterized in that it comprises a reflector which, in the stored position of the antenna, has its active face facing away from the support structure of the antenna, the rod of connection of the reflector with the deployment arm then being directed towards the top of the support structure, the articulation of this rod with the arm being at a degree of freedom in rotation, the deployment arm of the reflector being connected to the supporting structure the antenna by an articulation with at least one degree of freedom in rotation fixed to this structure, this arm being positioned between the reflector and the structure in the stored position of the antenna, the reflector then being applied against this structure.
  • the antenna 2 of the invention is fixed on the lateral face 3A of a support structure 3 supporting other devices not shown.
  • the source 4 of the antenna is fixed to the upper part of the structure 3.
  • the paraboloid reflector 5 of the antenna comprises at its rear face a radial fixing rod 6 integral with the rear face of the reflector (shell and / or all other rear structure).
  • the rod 6 is connected by a motorized articulation 7 (motorized by means of a leaf spring or a stepper motor) to a rotational degree of freedom at one end of the deployment arm 8 itself. reflector.
  • the other end of the arm 8 is connected by a hinge 9 to a secondary support 10, itself fixed on the structure 3.
  • the hinge 9 is at least one degree of freedom in rotation.
  • the hinge 9 is motorized and comprises one or two electric motors step-by-step, or a leaf spring (for a single degree of freedom in rotation).
  • the arm 8 is folded and is substantially parallel to the face 3A of the structure 3, the hinge 7 being pressed against the upper part of the face 3A.
  • the rod 6 and the reflector 5 are also pressed against this face 3A. In this position, the reflector 5 substantially does not extend beyond the sides of the face 3A.
  • the motorization - ensured by a spring (mechanical) or by a step-by-step motor (electric) - of the articulation 9 spreads the arm 8 of the face 3A , while that of the hinge 7 rotates the rod 6 which rotates about the axis of the hinge 7 (in figure 2 , the rod 6 is shown after being rotated by about 90 °).
  • Rod 6 rotates from its folded position ( figure 1 ) to the position of normal use of the reflector 5 (see Figures 3 and 4 ) at an angle of about 280 °, while the arm 8 rotates about 170 °.
  • the latter is oriented towards the Earth, while being, of course, positioned correctly with respect to the source 4.
  • the rotations of the arm 8 and the rod 6 can be synchronized, sequenced or simultaneous.

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerials With Secondary Devices (AREA)
  • Details Of Aerials (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
EP09173375.8A 2008-10-24 2009-10-19 Kompakte und robuste Antenne mit langer Brennweite, zur Prüfung auf der Prüfbank und Einbau in einem Satellit Active EP2190059B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0805922A FR2937800B1 (fr) 2008-10-24 2008-10-24 Antenne a longue focale, compacte, robuste et testable au sol, montee sur satellite

Publications (2)

Publication Number Publication Date
EP2190059A1 true EP2190059A1 (de) 2010-05-26
EP2190059B1 EP2190059B1 (de) 2014-05-14

Family

ID=40801827

Family Applications (1)

Application Number Title Priority Date Filing Date
EP09173375.8A Active EP2190059B1 (de) 2008-10-24 2009-10-19 Kompakte und robuste Antenne mit langer Brennweite, zur Prüfung auf der Prüfbank und Einbau in einem Satellit

Country Status (3)

Country Link
US (1) US8487830B2 (de)
EP (1) EP2190059B1 (de)
FR (1) FR2937800B1 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3047114A1 (fr) * 2016-01-22 2017-07-28 Thales Sa Ensemble reflecteur d'antenne a source fixe adaptee pour etre montee sur un satellite

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4462601A3 (de) 2010-12-15 2025-02-19 Planet Labs PBC Integriertes antennensystem zur abbildung von mikrosatelliten
EP3034412B1 (de) * 2014-12-16 2017-10-11 Ruag Space GmbH Stellmechanismus zum verstellen wenigstens eines triebwerks eines raumflugkörpers
JP6514366B2 (ja) 2015-02-24 2019-05-15 フラウンホーファー−ゲゼルシャフト・ツール・フェルデルング・デル・アンゲヴァンテン・フォルシュング・アインゲトラーゲネル・フェライン 集束アンテナを備えた集積型トランシーバ
US9878806B2 (en) 2015-03-09 2018-01-30 Space Systems/Loral, Llc On-orbit assembly of communication satellites
US10259599B2 (en) * 2015-12-08 2019-04-16 Space Systems/Loral, Llc Spacecraft with rigid antenna reflector deployed via linear extension boom
US10053240B1 (en) * 2016-05-20 2018-08-21 Space Systems/Loral, Llc Stowage, deployment and positioning of rigid antenna reflectors on a spacecraft
US10153559B1 (en) * 2016-06-23 2018-12-11 Harris Corporation Modular center fed reflector antenna system
US10800551B2 (en) * 2017-06-21 2020-10-13 Space Systems/Loral, Llc High capacity communication satellite
FR3086927B1 (fr) * 2018-10-04 2020-09-18 Thales Sa Dispositif de deploiement
CN114069188B (zh) * 2021-12-27 2024-06-04 浙江众星志连科技有限责任公司 一种皮纳卫星天线展开及锁紧装置

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2127624A (en) * 1982-09-22 1984-04-11 Rca Corp Antenna mounting system
US5257034A (en) * 1992-07-29 1993-10-26 Space Systems/Loral, Inc. Collapsible apparatus for forming a paraboloid surface
EP0704373A2 (de) * 1994-09-28 1996-04-03 Space Systems / Loral, Inc. Entfaltungsgelenkvorrichtung
US6424314B1 (en) * 2001-05-16 2002-07-23 Space Systems/Loral, Inc. Four axis boom for mounting reflector on satellite
WO2005097595A1 (en) * 2004-04-08 2005-10-20 Eads Astrium Limited Deployable boom

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2823182B1 (fr) * 2001-04-05 2004-06-04 Cit Alcatel Radiateur deployable pour engin spatial

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2127624A (en) * 1982-09-22 1984-04-11 Rca Corp Antenna mounting system
US5257034A (en) * 1992-07-29 1993-10-26 Space Systems/Loral, Inc. Collapsible apparatus for forming a paraboloid surface
EP0704373A2 (de) * 1994-09-28 1996-04-03 Space Systems / Loral, Inc. Entfaltungsgelenkvorrichtung
US6424314B1 (en) * 2001-05-16 2002-07-23 Space Systems/Loral, Inc. Four axis boom for mounting reflector on satellite
WO2005097595A1 (en) * 2004-04-08 2005-10-20 Eads Astrium Limited Deployable boom

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3047114A1 (fr) * 2016-01-22 2017-07-28 Thales Sa Ensemble reflecteur d'antenne a source fixe adaptee pour etre montee sur un satellite

Also Published As

Publication number Publication date
US20100103073A1 (en) 2010-04-29
US8487830B2 (en) 2013-07-16
EP2190059B1 (de) 2014-05-14
FR2937800B1 (fr) 2010-11-12
FR2937800A1 (fr) 2010-04-30

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