ES2044690T3 - Satelite de observacion de tipo geostacionario con sistema de maniobrade apogeo con ergoles liquidos y antenas huecas. - Google Patents

Satelite de observacion de tipo geostacionario con sistema de maniobrade apogeo con ergoles liquidos y antenas huecas.

Info

Publication number
ES2044690T3
ES2044690T3 ES91400488T ES91400488T ES2044690T3 ES 2044690 T3 ES2044690 T3 ES 2044690T3 ES 91400488 T ES91400488 T ES 91400488T ES 91400488 T ES91400488 T ES 91400488T ES 2044690 T3 ES2044690 T3 ES 2044690T3
Authority
ES
Spain
Prior art keywords
satellite
antennas
ergols
hollows
maneuvering
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
ES91400488T
Other languages
English (en)
Inventor
Patrick Maute
Alain Reboux
Bertrand Huet
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
Priority claimed from FR9002367A external-priority patent/FR2658783B1/fr
Priority claimed from FR9012126A external-priority patent/FR2667299B1/fr
Application filed by Airbus Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of ES2044690T3 publication Critical patent/ES2044690T3/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
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/281—Spin-stabilised spacecraft
    • 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
    • B64G1/1021—Earth observation 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
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/242—Orbits and trajectories
    • B64G1/2427—Transfer orbits
    • 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
    • B64G1/401—Liquid propellant rocket engines
    • 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
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/402—Propellant tanks; Feeding propellants
    • 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
    • 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
    • Y10S343/00—Communications: radio wave antennas
    • Y10S343/02—Satellite-mounted antenna

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Plasma & Fusion (AREA)
  • Details Of Aerials (AREA)
  • Radio Relay Systems (AREA)
  • Support Of Aerials (AREA)

Abstract

SATELITE (1) DESTINADO A SER SITUADO CON AUTOMATIZACION EN UNA ORBITA GEOESTACIONARIA QUE INCLUYE, COAXIALES A UN EJE DE AUTORROTACION (-Z+Z), UN CUERPO DE SATELITE (2) RODEADO POR UN GENERADOR SOLAR (3), AL MENOS DOS EQUIPOS (6, 12), UN SISTEMA DE MANIOBRA DE APOGEO (8) DISPUESTO SEGUN EL EJE Y UN JUEGO DE ANTENAS (7) QUE INCLUYE, AL MENOS, UNA ANTENA DE TRANSMISION DE IMAGENES (15), CARACTERIZADO PORQUE EL JUEGO DE ANTENA TIENE GLOBALMENTE LA FORMA DE UNA CORONA EN UNA DE LAS CARAS NORTE Y SUR DEL SATELITE, EN CUYO CENTRO SE HA DEJADO DESLIGADO UN ESPACIO CILINDRICO (14) SEGUN EL EJE DE AUTOMATIZACION PARA LA IMPLANTACION DE UNO DE LOS EQUIPOS, MIENTRAS QUE EL OTRO EQUIPO SE IMPLANTA EN LA OTRA DE LAS CARAS NORTE Y SUR.
ES91400488T 1990-02-26 1991-02-22 Satelite de observacion de tipo geostacionario con sistema de maniobrade apogeo con ergoles liquidos y antenas huecas. Expired - Lifetime ES2044690T3 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9002367A FR2658783B1 (fr) 1990-02-26 1990-02-26 Satellite d'observation de type geostationnaire a systeme de manóoeuvre d'apogee a ergols liquides et a antennes creuses.
FR9012126A FR2667299B1 (fr) 1990-10-02 1990-10-02 Satellite de type geostationnaire a systeme de manóoeuvre d'apogee a ergols liquides et a antennes creuses.

Publications (1)

Publication Number Publication Date
ES2044690T3 true ES2044690T3 (es) 1994-01-01

Family

ID=26227885

Family Applications (1)

Application Number Title Priority Date Filing Date
ES91400488T Expired - Lifetime ES2044690T3 (es) 1990-02-26 1991-02-22 Satelite de observacion de tipo geostacionario con sistema de maniobrade apogeo con ergoles liquidos y antenas huecas.

Country Status (6)

Country Link
US (1) US5169094A (es)
EP (1) EP0445010B1 (es)
JP (1) JP3122147B2 (es)
CA (1) CA2037008A1 (es)
DE (1) DE69100382T2 (es)
ES (1) ES2044690T3 (es)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2046021T3 (es) * 1990-02-26 1994-01-16 Aerospatiale Satelite de observacion de tipo geoestacionario con sistema de maniobra de apogeo de ergoles liquidos y con varias toberas.
FR2682931B1 (fr) * 1991-10-28 1994-01-28 Aerospatiale Ste Nationale Indle Vehicule spatial d'observation, notamment en infrarouges, a systeme de detecteurs refroidis connectes par des fils supraconducteurs.
FR2727934A1 (fr) * 1994-12-08 1996-06-14 Aerospatiale Satellite geostationnaire stabilise 3-axes a surveillance radar de son espace environnant
US5752676A (en) * 1996-08-06 1998-05-19 Ramot University Authority For Applied Research & Industrial Development Ltd. Spacecraft with integrated array of solar cells and electronically scannable antenna
RU2165379C1 (ru) * 2000-04-24 2001-04-20 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" им. С.П. Королева" Ракетный разгонный блок
RU2242405C2 (ru) * 2003-01-08 2004-12-20 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" им. С.П. Королева" Ракетный разгонный блок
RU2247063C2 (ru) * 2003-01-08 2005-02-27 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" им. С.П. Королева" Ракетный разгонный блок (варианты)
US7090171B2 (en) 2003-01-14 2006-08-15 Honeywell International, Inc. Momentum stabilized launch vehicle upper stage
US8639181B2 (en) * 2007-01-25 2014-01-28 The Boeing Company Lunar communications system
FR2919270B1 (fr) * 2007-07-24 2009-09-25 Thales Sa Dispositif de protection solaire pour instrument spatial
RU2376216C2 (ru) * 2007-11-14 2009-12-20 Федеральное государственное унитарное предприятие "Научно-исследовательский институт машиностроения" (ФГУП "НИИМаш") Двигательный модуль космического летательного аппарата
RU2421379C2 (ru) * 2010-06-02 2011-06-20 Александр Михайлович Гультяев Космический летательный аппарат
RU2421380C2 (ru) * 2010-06-07 2011-06-20 Александр Михайлович Гультяев Космический летательный аппарат
RU2420434C2 (ru) * 2010-07-06 2011-06-10 Александр Михайлович Гультяев Космический перевозчик
US8640994B1 (en) * 2010-09-27 2014-02-04 The Boeing Company Agile dedicated spacecraft for spinning microwave imagers and sounders
USD756886S1 (en) * 2014-03-18 2016-05-24 Planetary Resources Development Corp. Spacecraft system
CN104071354B (zh) * 2014-05-28 2016-07-20 上海微小卫星工程中心 一种卫星壳体及使用该壳体的卫星
CN104632814B (zh) * 2014-12-09 2016-08-24 上海复合材料科技有限公司 一种用于承力筒的胶接装配模
FR3041939B1 (fr) * 2015-10-02 2017-10-20 Airbus Defence & Space Sas Satellite comprenant un instrument optique de prise de vue
FR3041940B1 (fr) * 2015-10-02 2018-07-13 Airbus Defence And Space Sas Satellite a corps principal cylindrique, empilement comprenant un tel satellite et ensemble de lancement pour un tel satellite
US10306984B2 (en) * 2016-08-30 2019-06-04 The Boeing Company Toroidal support structures
US11104459B2 (en) * 2017-04-13 2021-08-31 Northrop Grumman Systems Corporation Systems for capturing a client vehicle
CN107284695A (zh) * 2017-06-19 2017-10-24 北京零壹空间科技有限公司 一种贮箱安装固定装置
CN117262238A (zh) 2017-07-21 2023-12-22 诺思路·格鲁曼系统公司 航天器服务装置及相关组件、系统和方法
US10085200B1 (en) 2017-09-29 2018-09-25 Star Mesh LLC Radio system using nodes with high gain antennas
JP2022517269A (ja) 2019-01-15 2022-03-07 ノースロップ グラマン システムズ コーポレーション 宇宙船作業用デバイス、ならびに関連の組立体、システム、および方法
CN109854596B (zh) * 2019-03-08 2021-02-09 北京航天自动控制研究所 一种飞行器光学头罩与舱体定位安装设备及安装方法
CN111409872B (zh) * 2020-03-06 2020-11-24 上海卫星工程研究所 适用于深空撞击器的一体式可分离连接安装支架
CN111409862B (zh) * 2020-03-10 2022-08-12 上海卫星工程研究所 卫星的载荷与星敏感器的安装结构及方法
CN111634444B (zh) * 2020-04-30 2021-12-07 航天东方红卫星有限公司 一种卫星载荷相机隔振机构行程保护工装及装配方法
US12371195B2 (en) 2020-05-04 2025-07-29 Northrop Grumman Systems Corporation Vehicle capture assemblies and related devices, systems, and methods
US11827386B2 (en) 2020-05-04 2023-11-28 Northrop Grumman Systems Corporation Vehicle capture assemblies and related devices, systems, and methods
US12338006B2 (en) 2022-11-18 2025-06-24 Northrop Grumman Systems Corporation Movable platforms for vehicle capture assemblies and related devices, assemblies, systems, and methods

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3758051A (en) * 1964-08-21 1973-09-11 Hughes Aircraft Co Velocity control and orientation of a spin-stabilized body
FR1427745A (fr) * 1964-11-13 1966-02-11 Thomson Houston Comp Francaise Perfectionnements aux antennes pour véhicules spatiaux
FR1524342A (fr) * 1967-03-31 1968-05-10 Labo Cent Telecommunicat Système de localisation et de mesure de phénomènes lumineux
GB1156891A (en) * 1967-06-20 1969-07-02 Hughes Aircraft Co Improvements in and relating to Switching and Power Phasing Apparatus for Automatically Forming and Despinning an Antenna Beam for a Spinning Body
US3817481A (en) * 1971-11-17 1974-06-18 Trw Inc Deployable solar array for a spin stabilized spacecraft
DE2642061C2 (de) * 1976-09-18 1983-11-24 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Lageregelungs- und Bahnänderungsverfahren für einen dreiachsenstabilisierbaren Satelliten, insbesondere für einen geostationären Satelliten und Einrichtung zur Durchführung des Verfahrens
US4305555A (en) * 1977-10-20 1981-12-15 Davis Charles E Solar energy system with relay satellite
US4343005A (en) * 1980-12-29 1982-08-03 Ford Aerospace & Communications Corporation Microwave antenna system having enhanced band width and reduced cross-polarization
US4753506A (en) * 1986-09-02 1988-06-28 Hughes Aircraft Company Off axis optical communication system
US5263666A (en) * 1988-12-16 1993-11-23 General Electric Co. Spacecraft with increased stationkeeping fuel load

Also Published As

Publication number Publication date
EP0445010B1 (fr) 1993-09-22
JP3122147B2 (ja) 2001-01-09
CA2037008A1 (en) 1991-08-27
JPH0550996A (ja) 1993-03-02
DE69100382D1 (de) 1993-10-28
DE69100382T2 (de) 1994-01-13
EP0445010A1 (fr) 1991-09-04
US5169094A (en) 1992-12-08

Similar Documents

Publication Publication Date Title
ES2044690T3 (es) Satelite de observacion de tipo geostacionario con sistema de maniobrade apogeo con ergoles liquidos y antenas huecas.
ATE43311T1 (de) Tetraeder-satellitenkonstellationen mit ununterbrochener ausleuchtzone.
ES2046021T3 (es) Satelite de observacion de tipo geoestacionario con sistema de maniobra de apogeo de ergoles liquidos y con varias toberas.
ES2071926T3 (es) Aparato de radiofrecuencia.
FR2628274B1 (fr) Systeme de communications avec des mobiles a l'aide de satellites
DE3065443D1 (en) Satellite earth observation system
ATE197861T1 (de) Übertragungsanordnung mit satelliten niedriger höhe und optimaler erdbeleuchtung für ein telekommunikationsnetz mit speicherung und durchschaltung
DE3773336D1 (de) Raumfahrzeug mit ausrichtanordnung einer antenne zur erde.
PRADHAN The Indian space program
PRITCHARD On-orbit checkout of satellites, volume 2. Part 3 of on-orbit checkout study(space maintenance)[Final Report]
EP0152221A3 (en) An earth terminal for satellite communication systems
Ahmed et al. Canadian solar array developments for space applications
POSPISIL et al. Compact space power station- Building up scenario(for solar energy transfer to lunar bases)
Hilton Electronics in space
FORWARD Twenty-first century space propulsion study(Final Report, 30 Jul. 1987-30 Apr. 1990)
MOBREM High-performance deployable structures for the support of high-concentration ratio solar array modules(Final Report)
Shaffer International coordination of and contributions to environmental satellite programs.
DEGRAAUW et al. The Scientific Importance of Submillimetre observations(conferences)
PRITCHARD et al. BRAVO economic study of LANDSAT follow-on[Final Report]
Powell et al. Space station design-Innovation and compromise
McKenna Atlantis to study sun's effect on atmosphere
Gal Activities on orbit and on celestial bodies- Two motions of peaceful uses?
Hueter Thermal/environmental control and life support system requirements for future space application
JANKOWITSCH New opportunities for international ventures
Sarles Jr et al. The Lincoln Experimental Satellites LES-8 and-9

Legal Events

Date Code Title Description
FG2A Definitive protection

Ref document number: 445010

Country of ref document: ES