ES2046021T3 - Satelite de observacion de tipo geoestacionario con sistema de maniobra de apogeo de ergoles liquidos y con varias toberas. - Google Patents

Satelite de observacion de tipo geoestacionario con sistema de maniobra de apogeo de ergoles liquidos y con varias toberas.

Info

Publication number
ES2046021T3
ES2046021T3 ES91400489T ES91400489T ES2046021T3 ES 2046021 T3 ES2046021 T3 ES 2046021T3 ES 91400489 T ES91400489 T ES 91400489T ES 91400489 T ES91400489 T ES 91400489T ES 2046021 T3 ES2046021 T3 ES 2046021T3
Authority
ES
Spain
Prior art keywords
satellite
ergols
liquid
observation
support
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
ES91400489T
Other languages
English (en)
Inventor
Patrick Maute
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 FR9002366A external-priority patent/FR2658782B1/fr
Priority claimed from FR9008969A external-priority patent/FR2664562B1/fr
Application filed by Airbus Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of ES2046021T3 publication Critical patent/ES2046021T3/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
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
    • 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
    • B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • B64G1/1021—Earth observation satellites
    • B64G1/1042—Earth observation satellites specifically adapted for meteorology
    • 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
    • B64G1/24—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
    • B64G1/22—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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/50—Feeding propellants using pressurised fluid to pressurise the propellants

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • General Engineering & Computer Science (AREA)
  • Plasma & Fusion (AREA)
  • Mechanical Engineering (AREA)
  • Plasma Technology (AREA)
  • Photovoltaic Devices (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Nozzles (AREA)
  • Details Of Aerials (AREA)

Abstract

SATELITE (1) DESTINADO A SER ESTABILIZADO CON AUTORROTACION 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), UN SISTEMA DE MANIOBRA DE APOGEO (8) DISPUESTO SEGUN EL EJE Y DOS EQUIPOS (7, 6) DISPUESTOS AXIALMENTE, CARACTERIZADO PORQUE EL SISTEMA DE MANIOBRA DE APOGEO INCLUYE EN OPOSICION A UNO DE LOS EQUIPOS UNA PLURALIDAD DE AL MENOS DOS TOBERAS (12) ORIENTADAS PARALELAMENTE AL EJE, PERO DECALADAS RESPECTO DE ESTE A UNA MISMA DISTANCIA (L), DISTRIBUIDAS CIRCUNFERENCIALMENTE DE MODO REGULAR ALREDEDOR DE OTRO DE LOS EQUIPOS, ESTANDO DICHAS TOBERAS CONECTADAS A UN MISMO SISTEMA DE ORIENTACION DE ERGOLES LIQUIDOS (20-30).
ES91400489T 1990-02-26 1991-02-22 Satelite de observacion de tipo geoestacionario con sistema de maniobra de apogeo de ergoles liquidos y con varias toberas. Expired - Lifetime ES2046021T3 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9002366A FR2658782B1 (fr) 1990-02-26 1990-02-26 Satellite d'observation de type geostationnaire a systeme de manóoeuvre d'apogee a ergols liquides et a plusieurs tuyeres.
FR9008969A FR2664562B1 (fr) 1990-07-13 1990-07-13 Satellite de type geostationnaire a systeme de manóoeuvre d'apogee a ergols liquides et a plusieurs tuyeres.

Publications (1)

Publication Number Publication Date
ES2046021T3 true ES2046021T3 (es) 1994-01-16

Family

ID=26227884

Family Applications (1)

Application Number Title Priority Date Filing Date
ES91400489T Expired - Lifetime ES2046021T3 (es) 1990-02-26 1991-02-22 Satelite de observacion de tipo geoestacionario con sistema de maniobra de apogeo de ergoles liquidos y con varias toberas.

Country Status (6)

Country Link
US (2) US6082678A (es)
EP (1) EP0445011B1 (es)
JP (1) JP3102578B2 (es)
CA (1) CA2037005A1 (es)
DE (1) DE69100603T2 (es)
ES (1) ES2046021T3 (es)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050109878A1 (en) * 2002-03-28 2005-05-26 Dutch Space B.V. Spacecraft and method for building such a spacecraft and an adapter to be used in such a spacecraft
GB2388580A (en) * 2002-05-15 2003-11-19 Astrium Ltd An arrangement of solar panels and a radiator on a spacecraft
US7896607B2 (en) * 2004-09-24 2011-03-01 Raytheon Company Method and system for adjusting a position of an object
US7223063B2 (en) * 2004-09-24 2007-05-29 Raytheon Company Method and system for adjusting a position of an object
US7762498B1 (en) * 2005-06-09 2010-07-27 Lockheed Martin Corporation Enhanced high-efficiency spacecraft propulsion system
US8640994B1 (en) * 2010-09-27 2014-02-04 The Boeing Company Agile dedicated spacecraft for spinning microwave imagers and sounders
CN102030112A (zh) * 2010-11-19 2011-04-27 哈尔滨工业大学 液体动量轮回路结合太阳电池阵实现卫星姿态控制和电能获取的一体化执行机构
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
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
WO2019018826A1 (en) 2017-07-21 2019-01-24 Nicholson James Garret SPACE VEHICLE MAINTENANCE DEVICES AND ASSEMBLIES, SYSTEMS, AND ASSOCIATED METHODS
US10913551B1 (en) * 2018-02-14 2021-02-09 Lockheed Martin Corporation Fault-tolerant scalable high thrust spacecraft propulsion
US11021273B1 (en) * 2018-05-03 2021-06-01 Space Systems/Loral, Llc Unified spacecraft propellant management system for chemical and electric propulsion
CN109506941B (zh) * 2018-11-20 2020-07-14 西安航天动力技术研究所 偏航俯仰发动机的变推力机构打开可靠性增长试验装置
US11492148B2 (en) 2019-01-15 2022-11-08 Northrop Grumman Systems Corporation Spacecraft servicing pods configured to perform servicing operations on target spacecraft and related devices, assemblies, systems, and methods
US11827386B2 (en) 2020-05-04 2023-11-28 Northrop Grumman Systems Corporation Vehicle capture assemblies and related devices, systems, and methods
RO135272A0 (ro) * 2021-06-08 2021-10-29 Petrică Lucian Georgescu Navetă spaţială cu circuit închis

Family Cites Families (13)

* 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
US3817477A (en) * 1971-07-06 1974-06-18 Trw Inc Deployable annular solar array
US3817481A (en) * 1971-11-17 1974-06-18 Trw Inc Deployable solar array for a spin stabilized spacecraft
FR2537544B1 (fr) * 1982-12-14 1985-07-19 Matra Procede et dispositif de propulsion pour satellites
US4880185A (en) * 1986-02-18 1989-11-14 Hughes Aircraft Company Low pressure reaction control propulsion system for a spacecraft
US4911385A (en) * 1987-04-30 1990-03-27 Agrawal Brij N Attitude pointing error correction system and method for geosynchronous satellites
US4842223A (en) * 1988-03-09 1989-06-27 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Hatch cover
US4961551A (en) * 1988-11-18 1990-10-09 Hughes Aircraft Company Stabilization of a spinning spacecraft of arbitary shape
US5263666A (en) * 1988-12-16 1993-11-23 General Electric Co. Spacecraft with increased stationkeeping fuel load
IT1237059B (it) * 1989-11-24 1993-05-13 Selenia Ind Elettroniche Sensore d'orizzonte per satellliti utilizzante superconduttore/i ad alta temperatura critica.
US5169094A (en) * 1990-02-26 1992-12-08 Aerospatiale Societe Nationale Industrielle Geostationary earth observation satellite incorporating liquid propellant apogee maneuver system and hollow antennas
US5546309A (en) * 1993-10-20 1996-08-13 The Charles Stark Draper Laboratory, Inc. Apparatus and method for autonomous satellite attitude sensing
FR2714357B1 (fr) * 1993-12-27 1996-03-22 Aerospatiale Procédé de minimisation, amortissement ou compensation des perturbations sur un satellite stabilisé par autorotation.

Also Published As

Publication number Publication date
JP3102578B2 (ja) 2000-10-23
EP0445011A1 (fr) 1991-09-04
US6264145B1 (en) 2001-07-24
JPH05105197A (ja) 1993-04-27
EP0445011B1 (fr) 1993-11-10
US6082678A (en) 2000-07-04
DE69100603T2 (de) 1994-03-10
CA2037005A1 (en) 1991-08-27
DE69100603D1 (de) 1993-12-16

Similar Documents

Publication Publication Date Title
ES2046021T3 (es) Satelite de observacion de tipo geoestacionario con sistema de maniobra de apogeo de ergoles liquidos y con varias toberas.
ES2044690T3 (es) Satelite de observacion de tipo geostacionario con sistema de maniobrade apogeo con ergoles liquidos y antenas huecas.
GB610143A (en) Improvements in and relating to aircraft
ES2042251T3 (es) Dispositivo para el control de la posicion por velas solares para satelite estabilizado alrededor de sus tres ejes.
DE3868292D1 (de) Hydrokultursystem.
GB2018211A (en) Satellite
ES2044473T3 (es) Sistema de control de posicion de satelite utilizando un anillo magne tico supraconductor.
JPS5421862A (en) Production of liquid crystal elements
ES2000033A6 (es) Composicion de bitionol sulfoxido porcedimiento para su fabricacion y metodo de utilizacion de aquella
JPS54159075A (en) Device for waterspout
GR3003077T3 (en) Spacecraft with an antenna earth pointing device
SE8505949D0 (sv) Anordning vid vextstod
JPS5564175A (en) Moving edge for reaper or mower
JPS5298488A (en) Solar cell plate change-over driving device for satellites
JPS55135710A (en) Vacuum package for electromagnetic interference measurement
JPS5419379A (en) Semiconductor device
Eder Lunar base logistics
JPS6430303A (en) Antenna system
DAVEY et al. A study of thrust-modulation techniques(Gas jet thrust controlling satellite attitude)
Borromee et al. The HM-7 engine of Ariane's third stage
JPS5531572A (en) Parts carrier
RUNCORN et al. Royal Society, Discussion on the Solar System: Chemistry as a Key to its Origin, London, England, July 15, 16, 1987, Proceedings
Heimlich et al. Life support in the Shuttle Era
JPS5282256A (en) Liquid crystal indicating cell
Shepelev et al. Effect of weightlessness on the water fern Azolla

Legal Events

Date Code Title Description
FG2A Definitive protection

Ref document number: 445011

Country of ref document: ES