FR2581615B1 - Satellite de telecommunications geostationnaire - Google Patents

Satellite de telecommunications geostationnaire

Info

Publication number
FR2581615B1
FR2581615B1 FR868606554A FR8606554A FR2581615B1 FR 2581615 B1 FR2581615 B1 FR 2581615B1 FR 868606554 A FR868606554 A FR 868606554A FR 8606554 A FR8606554 A FR 8606554A FR 2581615 B1 FR2581615 B1 FR 2581615B1
Authority
FR
France
Prior art keywords
telecommunications satellite
geostationary
geostationary telecommunications
satellite
telecommunications
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
FR868606554A
Other languages
English (en)
Other versions
FR2581615A1 (fr
Inventor
Eberhard Frisch
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 FR2581615A1 publication Critical patent/FR2581615A1/fr
Application granted granted Critical
Publication of FR2581615B1 publication Critical patent/FR2581615B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q19/00—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
    • H01Q19/10—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces
    • H01Q19/18—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces having two or more spaced reflecting surfaces
    • H01Q19/19—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces having two or more spaced reflecting surfaces comprising one main concave reflecting surface associated with an auxiliary reflecting surface
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • B64G1/1007—Communications satellites
    • 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
    • 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
    • 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
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Aerials With Secondary Devices (AREA)
  • Details Of Aerials (AREA)
FR868606554A 1985-05-10 1986-05-06 Satellite de telecommunications geostationnaire Expired - Lifetime FR2581615B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3516811A DE3516811C2 (de) 1985-05-10 1985-05-10 Geostationärer Nachrichtensatellit

Publications (2)

Publication Number Publication Date
FR2581615A1 FR2581615A1 (fr) 1986-11-14
FR2581615B1 true FR2581615B1 (fr) 1990-01-12

Family

ID=6270328

Family Applications (1)

Application Number Title Priority Date Filing Date
FR868606554A Expired - Lifetime FR2581615B1 (fr) 1985-05-10 1986-05-06 Satellite de telecommunications geostationnaire

Country Status (4)

Country Link
US (1) US4690354A (fr)
JP (1) JPH068120B2 (fr)
DE (1) DE3516811C2 (fr)
FR (1) FR2581615B1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5439190A (en) * 1991-04-22 1995-08-08 Trw Inc. Medium-earth-altitude satellite-based cellular telecommunications
US5433726A (en) * 1991-04-22 1995-07-18 Trw Inc. Medium-earth-altitude satellite-based cellular telecommunications system
FR2815323B1 (fr) * 2000-10-16 2003-01-31 Cit Alcatel Perfectionnements apportes aux satellites geostationnaires
US8403270B2 (en) * 2006-09-15 2013-03-26 The Boeing Company Canted solar array and method for using same
US9871292B2 (en) * 2015-08-05 2018-01-16 Harris Corporation Steerable satellite antenna assembly with fixed antenna feed and associated methods
JP7269328B2 (ja) * 2019-04-18 2023-05-08 株式会社Ｑｐｓ研究所 アンテナ装置及び宇宙航行体

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1393820A (en) * 1920-11-02 1921-10-18 Frank M Osborne Airplane
US3914768A (en) * 1974-01-31 1975-10-21 Bell Telephone Labor Inc Multiple-beam Cassegrainian antenna
NL7608162A (nl) * 1976-07-22 1978-01-24 Vaclav Josef Vokurka Antenne in het bijzonder voor meet- doeleinden.
FR2385233A1 (fr) * 1977-03-25 1978-10-20 Thomson Csf Structure d'antenne a reflecteurs et notamment a reflecteurs excentres, et equipements de detection electromagnetique et de telecommunications spatiales comportant une telle structure
FR2472509A1 (fr) * 1979-12-27 1981-07-03 Organisation Europ Rech Sp Configuration de satellite artificiel permettant un controle d'attitude continu suivant trois axes
FR2476018A1 (fr) * 1980-02-14 1981-08-21 Org Europeene De Rech Configuration de satellites pour mission geostationnaire
FR2517626A1 (fr) * 1981-12-04 1983-06-10 Europ Agence Spatiale Engin spatial orbital, notamment satellite, a missions multiples
DE3376549D1 (en) * 1983-09-03 1988-06-16 Erno Raumfahrttechnik Gmbh Satellite system with variable configuration

Also Published As

Publication number Publication date
DE3516811C2 (de) 1987-03-12
DE3516811A1 (de) 1986-11-13
US4690354A (en) 1987-09-01
FR2581615A1 (fr) 1986-11-14
JPS61261198A (ja) 1986-11-19
JPH068120B2 (ja) 1994-02-02

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Legal Events

Date Code Title Description
ST Notification of lapse
ST Notification of lapse