FR2592855B1 - Systeme orbital avec configurations a sonde remorquee et a propulsion electrodynamique, utilisation d'un tel systeme et procede de transfert entre les configurations - Google Patents

Systeme orbital avec configurations a sonde remorquee et a propulsion electrodynamique, utilisation d'un tel systeme et procede de transfert entre les configurations

Info

Publication number
FR2592855B1
FR2592855B1 FR8600540A FR8600540A FR2592855B1 FR 2592855 B1 FR2592855 B1 FR 2592855B1 FR 8600540 A FR8600540 A FR 8600540A FR 8600540 A FR8600540 A FR 8600540A FR 2592855 B1 FR2592855 B1 FR 2592855B1
Authority
FR
France
Prior art keywords
configurations
transferring
orbital
towed
probe
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
Application number
FR8600540A
Other languages
English (en)
Other versions
FR2592855A1 (fr
Inventor
Uwe Engelking
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.)
Agence Spatiale Europeenne
Original Assignee
Agence Spatiale Europeenne
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 Agence Spatiale Europeenne filed Critical Agence Spatiale Europeenne
Priority to FR8600540A priority Critical patent/FR2592855B1/fr
Priority to US07/002,034 priority patent/US4824051A/en
Publication of FR2592855A1 publication Critical patent/FR2592855A1/fr
Application granted granted Critical
Publication of FR2592855B1 publication Critical patent/FR2592855B1/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/14—Space shuttles

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Geophysics And Detection Of Objects (AREA)
FR8600540A 1986-01-16 1986-01-16 Systeme orbital avec configurations a sonde remorquee et a propulsion electrodynamique, utilisation d'un tel systeme et procede de transfert entre les configurations Expired FR2592855B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR8600540A FR2592855B1 (fr) 1986-01-16 1986-01-16 Systeme orbital avec configurations a sonde remorquee et a propulsion electrodynamique, utilisation d'un tel systeme et procede de transfert entre les configurations
US07/002,034 US4824051A (en) 1986-01-16 1987-01-12 Orbital system including a tethered satellite

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8600540A FR2592855B1 (fr) 1986-01-16 1986-01-16 Systeme orbital avec configurations a sonde remorquee et a propulsion electrodynamique, utilisation d'un tel systeme et procede de transfert entre les configurations

Publications (2)

Publication Number Publication Date
FR2592855A1 FR2592855A1 (fr) 1987-07-17
FR2592855B1 true FR2592855B1 (fr) 1988-03-18

Family

ID=9331161

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8600540A Expired FR2592855B1 (fr) 1986-01-16 1986-01-16 Systeme orbital avec configurations a sonde remorquee et a propulsion electrodynamique, utilisation d'un tel systeme et procede de transfert entre les configurations

Country Status (2)

Country Link
US (1) US4824051A (fr)
FR (1) FR2592855B1 (fr)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5082211A (en) * 1990-10-31 1992-01-21 Teledyne Industries, Inc. Method and apparatus for mitigating space debris
IT1241836B (it) * 1990-11-30 1994-02-01 Proel Tecnologie Spa Dispositivo a cannone elettronico per il controllo del potenziale di un corpo nello spazio.
US5762298A (en) * 1991-03-27 1998-06-09 Chen; Franklin Y. K. Use of artificial satellites in earth orbits adaptively to modify the effect that solar radiation would otherwise have on earth's weather
US5321336A (en) * 1991-11-26 1994-06-14 Proel Technologie S.P.A. Electron gun device for controlling the potential of a body in space
DE4234875C2 (de) * 1992-10-16 1994-10-06 Deutsche Forsch Luft Raumfahrt Vorrichtung zur Kopplung von mindestens zwei Raumfahrtgeräten und Verwendung der Vorrichtung zur Reparatur von Seilbeschädigungen
US5760506A (en) * 1995-06-07 1998-06-02 The Boeing Company Flywheels for energy storage
US5865401A (en) * 1996-08-29 1999-02-02 Space Systems/Loral, Inc. Tethered space platform assembly for isolation orbiting
US6173922B1 (en) * 1997-04-22 2001-01-16 Robert P. Hoyt Failure resistant multiline tether
US6116544A (en) * 1997-09-12 2000-09-12 Tethers Unlimited, Inc. Electrodynamic tether and method of use
US6419191B1 (en) * 1997-09-12 2002-07-16 Robert P. Hoyt Electrodynamic tether control
US6290186B1 (en) * 1999-10-22 2001-09-18 Robert P. Hoyt Planar hoytether failure resistant multiline tether
US6577130B1 (en) 2000-05-31 2003-06-10 Sri International System and method for sensing and controlling potential differences between a space object and its space plasma environment using micro-fabricated field emission devices
WO2001092897A2 (fr) * 2000-05-31 2001-12-06 Sri International Systemes et procedes mettant en application des dispositifs d'emission de champ microfabriques afin de detecter et de controler des differences potentielles entre un objet spatial et son environnement plasmatique spatial, d'emettre une charge depuis un objet spatial et s'utilisant avec un filin electrodynamique pour regler
US6459206B1 (en) 2000-05-31 2002-10-01 Sri International System and method for adjusting the orbit of an orbiting space object using an electrodynamic tether and micro-fabricated field emission device
US6386484B1 (en) * 2000-09-08 2002-05-14 Robert P. Hoyt Failure resistant multiline tether
US6260807B1 (en) * 2000-09-08 2001-07-17 Robert P. Hoyt Failure resistant multiline tether
US6431497B1 (en) * 2000-09-08 2002-08-13 Robert P. Hoyt Failure resistant multiline tether
US6286788B1 (en) * 2000-09-08 2001-09-11 Robert P. Hoyt Alternate interconnection hoytether failure resistant multiline tether
US6942186B1 (en) 2001-03-07 2005-09-13 Star Technology And Research, Inc. Method and apparatus for propulsion and power generation using spinning electrodynamic tethers
US6758443B1 (en) 2001-03-07 2004-07-06 Tether Applications, Inc. Method for observing and stabilizing electrodynamic tethers
US6830222B1 (en) * 2002-03-21 2004-12-14 Global Aerospace Corporation Balloon device for lowering space object orbits
FR2838102B1 (fr) 2002-04-08 2004-11-26 Agence Spatiale Europeenne Systeme de propulsion combine destine a un engin spatial
US7118074B1 (en) * 2003-10-17 2006-10-10 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Electrodynamic tether
US7641151B2 (en) * 2006-03-02 2010-01-05 Pekka Janhunen Electric sail for producing spacecraft propulsion
US11724836B2 (en) * 2013-03-15 2023-08-15 Arthur M Dula Tether for spacecraft reaction control system
CN106855690B (zh) * 2016-11-24 2020-04-03 西北工业大学 空间绳系机器人近距离抓捕后回收目标的自适应控制方法
CN111216925B (zh) * 2020-02-13 2022-11-11 西北工业大学 一种共面椭圆轨道间的绳系卫星转移轨道设计方法
CN116039970B (zh) * 2023-01-17 2024-05-10 北京科技大学 一种最优的匀速-减速式绳系卫星系统分离方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3241142A (en) * 1962-12-28 1966-03-15 Litton Systems Inc Gravity stabilized satellite
US3582016A (en) * 1967-10-03 1971-06-01 Bernard C Sherman Satellite attitude control mechanism and method
US3532298A (en) * 1967-10-31 1970-10-06 Us Navy Method for deploying and stabilizing orbiting structures
US4097010A (en) * 1975-10-08 1978-06-27 Smithsonian Institution Satellite connected by means of a long tether to a powered spacecraft
US4083520A (en) * 1976-11-08 1978-04-11 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Tetherline system for orbiting satellites
US4580747A (en) * 1983-03-15 1986-04-08 Jerome Pearson Method and apparatus for orbital plane changing

Also Published As

Publication number Publication date
US4824051A (en) 1989-04-25
FR2592855A1 (fr) 1987-07-17

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Legal Events

Date Code Title Description
ER Errata listed in the french official journal (bopi)

Free format text: 29/87

ST Notification of lapse