EP1600728B1 - Engin volant pour l'observation du sol - Google Patents

Engin volant pour l'observation du sol Download PDF

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Publication number
EP1600728B1
EP1600728B1 EP05291021A EP05291021A EP1600728B1 EP 1600728 B1 EP1600728 B1 EP 1600728B1 EP 05291021 A EP05291021 A EP 05291021A EP 05291021 A EP05291021 A EP 05291021A EP 1600728 B1 EP1600728 B1 EP 1600728B1
Authority
EP
European Patent Office
Prior art keywords
flying object
elongate body
motor
lift
nozzles
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.)
Active
Application number
EP05291021A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP1600728A1 (fr
Inventor
Bernard Teneze
Michel Blin
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.)
MBDA France SAS
Original Assignee
MBDA France 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
Application filed by MBDA France SAS filed Critical MBDA France SAS
Publication of EP1600728A1 publication Critical patent/EP1600728A1/fr
Application granted granted Critical
Publication of EP1600728B1 publication Critical patent/EP1600728B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • F42B12/365—Projectiles transmitting information to a remote location using optical or electronic means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust

Definitions

  • the flying vehicle 1 can be propelled and directed on this target 21, by the rear 2R of the elongate body 2, or by the nozzles 4 and 6 in positions 7 and 8 (embodiment examples I and IV), either by the fixed nozzles 9 and 10 (embodiment II), or else by the additional propellant 11 and the nozzle 13 (embodiment III) ).
  • a recognition and attack process which more specifically corresponds to a bell-destroying fire of a masked target whose existence was probable, is illustrated in FIG.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Geophysics And Detection Of Objects (AREA)
  • Jib Cranes (AREA)
  • Earth Drilling (AREA)
  • Investigating, Analyzing Materials By Fluorescence Or Luminescence (AREA)
  • Analysing Materials By The Use Of Radiation (AREA)
EP05291021A 2004-05-27 2005-05-12 Engin volant pour l'observation du sol Active EP1600728B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0405719 2004-05-27
FR0405719A FR2870932B1 (fr) 2004-05-27 2004-05-27 Engin volant pour l'observation du sol

Publications (2)

Publication Number Publication Date
EP1600728A1 EP1600728A1 (fr) 2005-11-30
EP1600728B1 true EP1600728B1 (fr) 2006-11-02

Family

ID=34942274

Family Applications (1)

Application Number Title Priority Date Filing Date
EP05291021A Active EP1600728B1 (fr) 2004-05-27 2005-05-12 Engin volant pour l'observation du sol

Country Status (13)

Country Link
US (1) US7763834B2 (es)
EP (1) EP1600728B1 (es)
JP (1) JP4823219B2 (es)
KR (1) KR101287920B1 (es)
CN (1) CN100467999C (es)
AT (1) ATE344434T1 (es)
DE (1) DE602005000222T2 (es)
ES (1) ES2274506T3 (es)
FR (1) FR2870932B1 (es)
IL (1) IL176804A (es)
NO (1) NO333969B1 (es)
WO (1) WO2006000662A1 (es)
ZA (1) ZA200607459B (es)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007021112B3 (de) * 2007-05-05 2008-07-31 Lfk-Lenkflugkörpersysteme Gmbh Verfahren zur Vergrößerung des Aufklärungsradius eines Kampfhubschraubers, sowie Aufklärungsflugkörper und Kampfhubschrauber zur Durchführung des Verfahrens
JP5279523B2 (ja) * 2009-01-22 2013-09-04 三菱電機株式会社 姿勢計算装置及び誘導装置及び姿勢計算装置の姿勢計算方法及び姿勢計算装置の姿勢計算プログラム
US8878110B2 (en) * 2010-12-14 2014-11-04 Raytheon Company Projectile that includes propulsion system and launch motor on opposing sides of payload and method
FR2970702B1 (fr) * 2011-01-26 2013-05-10 Astrium Sas Procede et systeme de pilotage d'un engin volant a propulseur arriere
KR101917785B1 (ko) * 2016-10-26 2019-01-29 한국항공우주연구원 관측용 무동력형 비행 유닛
CN109141144B (zh) * 2018-09-29 2024-02-09 中国空空导弹研究院 一种红外制导导弹破碎型抛离罩
CN113776386B (zh) * 2020-06-10 2023-05-09 北京机械设备研究所 舰载垂直发射载荷的近距投放方法

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB751840A (en) 1951-07-06 1956-07-04 Armstrong Whitworth Co Eng Improvements relating to self-projected missiles
US3185096A (en) * 1959-08-31 1965-05-25 Roland G Dandelin Thrust reversal unit for rocket motor
FR1288750A (fr) * 1960-12-14 1962-03-30 Snecma Plate-forme sustentée par réaction, à poussée tarée, utilisée notamment au déminage
US3233548A (en) * 1963-11-12 1966-02-08 Canrad Prec Ind Inc Dirigible aerial torpedo
US3806064A (en) * 1968-10-03 1974-04-23 A Parilla Missile configurations, controls and utilization techniques
GB1284487A (en) * 1970-02-24 1972-08-09 Mullard Ltd Improvements in or relating to scanning and imaging systems
US3979086A (en) * 1974-11-08 1976-09-07 The United States Of America As Represented By The Secretary Of The Army Rocketed data communication system
NZ198917A (en) * 1980-11-14 1985-01-31 Commw Of Australia Rocket controlled by spoiler tabs in exhaust
DE3313648A1 (de) * 1983-04-15 1984-10-18 Diehl GmbH & Co, 8500 Nürnberg Verfahren zur echtzeit-gelaendeaufklaerung mittels eines sensors und einrichtung zum ausueben des verfahrens
FR2558585B1 (fr) * 1984-01-19 1987-10-23 Stauff Emile Sous-munitions largables pour projectile, notamment antichar
USH236H (en) * 1986-07-14 1987-03-03 The United States Of America As Represented By The Secretary Of The Army Asymmetric side-exhausting nozzles
JP2588739B2 (ja) * 1988-02-23 1997-03-12 防衛庁技術研究本部長 ロケットの飛翔方向制御装置
US4913379A (en) * 1988-02-23 1990-04-03 Japan as represented by Director General, Technical Research and Development Institute, Japan Defence Agency Rocket flight direction control system
JPH0331698A (ja) * 1989-06-28 1991-02-12 Boeing Co:The 光ファイバ誘導弾装置
DE4132233C2 (de) * 1990-11-22 2003-03-06 Rheinmetall W & M Gmbh Panzerabwehrraketensystem
FR2699610B1 (fr) * 1992-12-22 1995-02-10 Aerospatiale Dispositif d'actionnement d'un organe mécanique, notamment pour le pilotage en force d'un missile, et missile équipé dudit dispositif.
US5456425A (en) * 1993-11-04 1995-10-10 Aerojet General Corporation Multiple pintle nozzle propulsion control system
GB9501594D0 (en) * 1995-01-27 1995-11-08 British Aerospace Tethered missile system
JP3075343B2 (ja) * 1997-06-24 2000-08-14 防衛庁技術研究本部長 飛しょう体
JP3291542B2 (ja) * 1999-07-08 2002-06-10 防衛庁技術研究本部長 並進・姿勢制御装置
US6705573B2 (en) * 1999-12-30 2004-03-16 Advanced Aerospace Technologies, Inc. Survivability and mission flexibility enhancements for reconnaissance aircraft

Also Published As

Publication number Publication date
IL176804A (en) 2011-02-28
CN1961194A (zh) 2007-05-09
ATE344434T1 (de) 2006-11-15
EP1600728A1 (fr) 2005-11-30
WO2006000662A1 (fr) 2006-01-05
US7763834B2 (en) 2010-07-27
KR101287920B1 (ko) 2013-07-18
ES2274506T3 (es) 2007-05-16
NO333969B1 (no) 2013-11-04
DE602005000222D1 (de) 2006-12-14
JP2008500507A (ja) 2008-01-10
DE602005000222T2 (de) 2007-09-06
CN100467999C (zh) 2009-03-11
NO20065758L (no) 2006-12-13
ZA200607459B (en) 2007-12-27
FR2870932A1 (fr) 2005-12-02
US20080245256A1 (en) 2008-10-09
KR20070015371A (ko) 2007-02-02
FR2870932B1 (fr) 2006-08-11
IL176804A0 (en) 2006-10-31
JP4823219B2 (ja) 2011-11-24

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