EP2101139A3 - Guided missile - Google Patents

Guided missile Download PDF

Info

Publication number
EP2101139A3
EP2101139A3 EP09002986.9A EP09002986A EP2101139A3 EP 2101139 A3 EP2101139 A3 EP 2101139A3 EP 09002986 A EP09002986 A EP 09002986A EP 2101139 A3 EP2101139 A3 EP 2101139A3
Authority
EP
European Patent Office
Prior art keywords
unit
guided missile
missile
longitudinal direction
guided
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.)
Granted
Application number
EP09002986.9A
Other languages
German (de)
French (fr)
Other versions
EP2101139A2 (en
EP2101139B1 (en
Inventor
Peter Gerd Fisch
Michael Dr. Gross
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.)
Diehl BGT Defence GmbH and Co KG
Original Assignee
Diehl BGT Defence GmbH and Co KG
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 Diehl BGT Defence GmbH and Co KG filed Critical Diehl BGT Defence GmbH and Co KG
Publication of EP2101139A2 publication Critical patent/EP2101139A2/en
Publication of EP2101139A3 publication Critical patent/EP2101139A3/en
Application granted granted Critical
Publication of EP2101139B1 publication Critical patent/EP2101139B1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/10—Missiles having a trajectory only in the air

Abstract

Es wird ein Lenkflugkörper (1,1') mit einer Sensoreinheit (5), mit einer Antriebseinheit (7) und mit einer Nutzlasteinheit (8) angegeben, wobei eine die Außenkontur bildende, sich entlang einer Längsrichtung (4) erstreckende Flugkörperhülle (3) umfasst ist, die zur Aufnahme der Sensoreinheit (5), der Antriebseinheit (7) und der Nutzlasteinheit (8) ausgebildet ist, und wobei wenigstens zwei der Einheiten (5,7,8) in Längsrichtung (4) nebeneinander anbringbar sind. Der Lenkflugkörper (1,1') zeichnet sich gegenüber herkömmlichen Lenkflugkörpern durch eine erhöhte Modularität und somit durch eine erhöhte Flexibilität hinsichtlich verschiedener Einsatz-Szenarien aus.

Figure imgaf001
The invention relates to a guided missile (1, 1 ') having a sensor unit (5), a drive unit (7) and a payload unit (8), wherein a missile shell (3) forming the outer contour and extending along a longitudinal direction (4) is provided. is formed, which is adapted to receive the sensor unit (5), the drive unit (7) and the payload unit (8), and wherein at least two of the units (5,7,8) in the longitudinal direction (4) are mounted side by side. The guided missile (1,1 ') is distinguished from conventional guided missiles by an increased modularity and thus by an increased flexibility with respect to different deployment scenarios.
Figure imgaf001
EP09002986.9A 2008-03-13 2009-03-03 Guided missile Expired - Fee Related EP2101139B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102008014257A DE102008014257B4 (en) 2008-03-13 2008-03-13 Missile

Publications (3)

Publication Number Publication Date
EP2101139A2 EP2101139A2 (en) 2009-09-16
EP2101139A3 true EP2101139A3 (en) 2013-05-29
EP2101139B1 EP2101139B1 (en) 2015-06-10

Family

ID=40578877

Family Applications (1)

Application Number Title Priority Date Filing Date
EP09002986.9A Expired - Fee Related EP2101139B1 (en) 2008-03-13 2009-03-03 Guided missile

Country Status (4)

Country Link
US (1) US7893390B2 (en)
EP (1) EP2101139B1 (en)
DE (1) DE102008014257B4 (en)
IL (1) IL197503A (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015012970A1 (en) * 2015-10-07 2017-04-13 Mbda Deutschland Gmbh Function-oriented and reconfigurable missile
US9659502B1 (en) * 2015-12-18 2017-05-23 International Business Machines Corporation Drone range extension via host vehicles
US10281254B2 (en) 2016-09-20 2019-05-07 Rosemount Aerospace Inc. Phased array LIDAR in ordnance control
US20190176983A1 (en) * 2017-10-27 2019-06-13 Brian D. Darnell Rapid aerial deployed drone
RU2749928C1 (en) * 2020-05-13 2021-06-21 Акционерное общество «Информационные спутниковые системы» имени академика М.Ф. Решетнёва» Spacecraft
EP4060282B1 (en) * 2021-03-17 2023-10-25 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Missile having a body forming an airfoil at an angle oblique to the longitudinal axis of the missile

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4447025A (en) * 1981-08-14 1984-05-08 Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung Carrier for a dropload to be dropped from an aircraft
US4623106A (en) * 1984-10-25 1986-11-18 The United States Of America As Represented By The Secretary Of The Navy Reentry vehicle having active control and passive design modifications
DE3826702A1 (en) * 1988-08-05 1990-02-15 Aris Spa CONTROL, CONTROL AND DRIVE UNIT, ESPECIALLY FOR BALLISTIC AIRCRAFT
US20060016930A1 (en) * 2004-07-09 2006-01-26 Steve Pak Sky hopper
WO2006112578A1 (en) * 2005-04-20 2006-10-26 Won-Sup Oh Vertical take-off and landing aircraft
DE102005060369A1 (en) * 2005-12-16 2007-07-05 Airbus Deutschland Gmbh Aircraft for civil aviation, has module carrier accommodating several module elements such that each module element includes integrated system element
WO2008000203A1 (en) * 2006-06-26 2008-01-03 Burkhard Wiggerich Aircraft

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL98928C (en) * 1958-02-25
US4142695A (en) * 1971-10-27 1979-03-06 Raytheon Company Vehicle guidance system
DE2904749C2 (en) * 1979-02-08 1984-01-05 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Missile in the manner of a drone
US4364530A (en) * 1980-09-08 1982-12-21 The United States Of America As Represented By The Secretary Of The Navy Propulsion/control modular booster
US4899956A (en) * 1988-07-20 1990-02-13 Teleflex, Incorporated Self-contained supplemental guidance module for projectile weapons
DE3917111A1 (en) * 1989-05-26 1990-11-29 Dornier Gmbh REMOTE-CONTROLLED AIRCRAFT
DE3934834A1 (en) * 1989-10-19 1991-04-25 Messerschmitt Boelkow Blohm Guided missile housing assembly - is made from two halves fastened together by strips which form guides for control cables
US5267885A (en) * 1991-08-20 1993-12-07 Centuri Corporation Model rocket kit structure
US5211356A (en) * 1991-08-30 1993-05-18 Texas Instruments Incorporated Method and apparatus for rejecting trackable subimages
US5425514A (en) * 1993-12-29 1995-06-20 Raytheon Company Modular aerodynamic gyrodynamic intelligent controlled projectile and method of operating same
US5379968A (en) * 1993-12-29 1995-01-10 Raytheon Company Modular aerodynamic gyrodynamic intelligent controlled projectile and method of operating same
US5615846A (en) * 1994-11-04 1997-04-01 Gec Marconi Dynamics Inc. Extendable wing for guided missles and munitions
US6056237A (en) * 1997-06-25 2000-05-02 Woodland; Richard L. K. Sonotube compatible unmanned aerial vehicle and system
DE19828645C1 (en) * 1998-06-26 1999-11-18 Buck Werke Gmbh & Co I K Guided missile for fixed or moving targets
US6494140B1 (en) * 1999-04-22 2002-12-17 Lockheed Martin Corporation Modular rocket boosted penetrating warhead
DE102005042484B4 (en) * 2005-09-07 2012-01-12 Lfk-Lenkflugkörpersysteme Gmbh Unmanned gliding missile

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4447025A (en) * 1981-08-14 1984-05-08 Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung Carrier for a dropload to be dropped from an aircraft
US4623106A (en) * 1984-10-25 1986-11-18 The United States Of America As Represented By The Secretary Of The Navy Reentry vehicle having active control and passive design modifications
DE3826702A1 (en) * 1988-08-05 1990-02-15 Aris Spa CONTROL, CONTROL AND DRIVE UNIT, ESPECIALLY FOR BALLISTIC AIRCRAFT
US20060016930A1 (en) * 2004-07-09 2006-01-26 Steve Pak Sky hopper
WO2006112578A1 (en) * 2005-04-20 2006-10-26 Won-Sup Oh Vertical take-off and landing aircraft
DE102005060369A1 (en) * 2005-12-16 2007-07-05 Airbus Deutschland Gmbh Aircraft for civil aviation, has module carrier accommodating several module elements such that each module element includes integrated system element
WO2008000203A1 (en) * 2006-06-26 2008-01-03 Burkhard Wiggerich Aircraft

Also Published As

Publication number Publication date
EP2101139A2 (en) 2009-09-16
US7893390B2 (en) 2011-02-22
DE102008014257A1 (en) 2009-09-17
IL197503A0 (en) 2009-12-24
US20090230234A1 (en) 2009-09-17
DE102008014257B4 (en) 2009-12-03
EP2101139B1 (en) 2015-06-10
IL197503A (en) 2014-06-30

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