ATE107903T1 - Satellit und verfahren, um einen satelliten in eine umlaufbahn mit hilfe der schwerkraft zu bringen. - Google Patents

Satellit und verfahren, um einen satelliten in eine umlaufbahn mit hilfe der schwerkraft zu bringen.

Info

Publication number
ATE107903T1
ATE107903T1 AT90402056T AT90402056T ATE107903T1 AT E107903 T1 ATE107903 T1 AT E107903T1 AT 90402056 T AT90402056 T AT 90402056T AT 90402056 T AT90402056 T AT 90402056T AT E107903 T1 ATE107903 T1 AT E107903T1
Authority
AT
Austria
Prior art keywords
orbit
satellite
gravity
placing
sphere
Prior art date
Application number
AT90402056T
Other languages
English (en)
Inventor
Jean-Francois Dulck
Original Assignee
Centre Nat Etd Spatiales
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 Nat Etd Spatiales filed Critical Centre Nat Etd Spatiales
Application granted granted Critical
Publication of ATE107903T1 publication Critical patent/ATE107903T1/de

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/242Orbits and trajectories
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/242Orbits and trajectories
    • B64G1/2427Transfer orbits
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B7/00Radio transmission systems, i.e. using radiation field
    • H04B7/14Relay systems
    • H04B7/15Active relay systems
    • H04B7/185Space-based or airborne stations; Stations for satellite systems
    • H04B7/195Non-synchronous stations

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • General Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • Physics & Mathematics (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Signal Processing (AREA)
  • Radio Relay Systems (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Crystals, And After-Treatments Of Crystals (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)
  • Electrotherapy Devices (AREA)
  • Fertilizing (AREA)
AT90402056T 1989-07-19 1990-07-17 Satellit und verfahren, um einen satelliten in eine umlaufbahn mit hilfe der schwerkraft zu bringen. ATE107903T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8909713A FR2650135B1 (fr) 1989-07-19 1989-07-19 Satellite et procede de mise en orbite par assistance gravitationnelle
US07/646,426 US5507454A (en) 1989-07-19 1991-01-28 Satellite and method to place this satellite in orbit by gravitational assistance

Publications (1)

Publication Number Publication Date
ATE107903T1 true ATE107903T1 (de) 1994-07-15

Family

ID=26227481

Family Applications (1)

Application Number Title Priority Date Filing Date
AT90402056T ATE107903T1 (de) 1989-07-19 1990-07-17 Satellit und verfahren, um einen satelliten in eine umlaufbahn mit hilfe der schwerkraft zu bringen.

Country Status (5)

Country Link
US (1) US5507454A (de)
EP (1) EP0409721B1 (de)
AT (1) ATE107903T1 (de)
DE (1) DE69010286T2 (de)
FR (1) FR2650135B1 (de)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5681011A (en) * 1993-08-24 1997-10-28 Orbital Sciences Corporation Method for injecting payloads into orbit
US6400926B1 (en) * 1994-06-22 2002-06-04 Ericsson Ge Mobile Communications Inc. Radiocommunication system using geostationary and non-geostationary satellites
US5833175A (en) * 1995-12-22 1998-11-10 Hughes Electronics Corporation Spacecraft with large east-west dimensions
US6223019B1 (en) 1996-03-14 2001-04-24 Sirius Satellite Radio Inc. Efficient high latitude service area satellite mobile broadcasting systems
FR2747102B1 (fr) * 1996-04-05 1998-06-26 Europ Propulsion Procede et systeme de mise en orbite d'un vehicule spatial avec des propulseurs a forte impulsion specifique
FR2757824B1 (fr) * 1996-12-31 1999-03-26 Europ Propulsion Procede et systeme de lancement de satellites sur des orbites non coplanaires en utilisant l'assistance gravitationnelle lunaire
AU6649798A (en) * 1997-02-04 1998-08-25 Edward A. Belbruno New procedure for generating operational ballistic capture transfer using a computer implemented process
US6023616A (en) * 1998-03-10 2000-02-08 Cd Radio Inc. Satellite broadcast receiver system
WO1998040675A1 (en) 1997-03-14 1998-09-17 Cove Corporation Plated projectile for use in subsonic ammunition
US6097997A (en) * 1997-03-25 2000-08-01 Galaxy Development, Llc Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same
AU7357198A (en) * 1997-03-25 1998-10-20 Edward A. Belbruno Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same
AU738202B2 (en) * 1997-04-24 2001-09-13 Galaxy Development, Llc. Satellite inclination changes using weak stability boundaries
US7198230B2 (en) * 1997-10-14 2007-04-03 The Directv Group, Inc. Method and system for maximizing satellite constellation coverage
US6116545A (en) * 1998-04-09 2000-09-12 Hughes Electronics Corporation Free return lunar flyby transfer method for geosynchronous satellites
US6149103A (en) * 1998-04-09 2000-11-21 Hughes Electronics Corporation Free return lunar flyby transfer method for geosynchronous satellites havint multiple perilune stages
US6385512B1 (en) 1999-04-16 2002-05-07 Galaxy Development Llc System and method of a ballistic capture transfer to L4, L5
US20040097304A1 (en) * 2002-11-18 2004-05-20 Jerry Sharp Flexible football tee
US7219858B2 (en) * 2004-07-06 2007-05-22 The Johns Hopkins University Method for deploying multiple spacecraft
US20120119034A1 (en) * 2009-07-02 2012-05-17 Space Systems/Loral, Inc. Deorbiting a Spacecraft from a Highly Inclined Elliptical Orbit
RU2486676C2 (ru) * 2010-12-20 2013-06-27 Государственное образовательное учреждение высшего профессионального образования Московский технический университет связи и информации (ГОУ ПВО МТУСИ) Способ объединения спутниковых систем связи
US8655589B2 (en) * 2012-01-25 2014-02-18 Mitsubishi Electric Research Laboratories, Inc. System and method for controlling motion of spacecrafts
US9114893B2 (en) * 2012-07-26 2015-08-25 Mitsubishi Electric Research Laboratories, Inc. System and method for estimating states of spacecraft in planet-moon environment
US9284068B2 (en) * 2014-04-08 2016-03-15 The Boeing Company Fast-low energy transfer to Earth-Moon Lagrange point L2
FR3020348B1 (fr) * 2014-04-24 2016-05-13 Snecma Procede de deploiement d'une constellation de satellites
US9550585B2 (en) * 2014-06-09 2017-01-24 Space Systems/Loral, Llc Highly inclined elliptical orbit de-orbit techniques
US9365299B2 (en) * 2014-06-09 2016-06-14 Space Systems/Loral, Llc Highly inclined elliptical orbit launch and orbit acquisition techniques
CN109080854B (zh) * 2018-07-19 2021-06-18 北京空间技术研制试验中心 航天器返回预定落点的大椭圆轨道变轨规划方法
CN113978768B (zh) * 2021-10-28 2024-01-05 中国西安卫星测控中心 利用月球引力辅助部署Retro-GEO轨道设计方法

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
UST100604I4 (en) * 1979-01-29 1981-05-05 Method of placing a spacecraft into final earth orbit or earth escape trajectory
FR88335E (fr) * 1958-09-04 1967-01-20 Dispositif pour la mise en rotation du plan de l'orbite d'un mobile en gravitation ainsi que mobiles tels que satellites, pourvus du présent dispositif ou dispositif similaire
US3995801A (en) * 1974-07-05 1976-12-07 Rca Corporation Method of storing spare satellites in orbit
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

Also Published As

Publication number Publication date
FR2650135B1 (fr) 1994-05-20
EP0409721B1 (de) 1994-06-29
FR2650135A1 (fr) 1991-01-25
DE69010286T2 (de) 1995-01-05
DE69010286D1 (de) 1994-08-04
EP0409721A1 (de) 1991-01-23
US5507454A (en) 1996-04-16

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Legal Events

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RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties