DE59400761D1 - Mittels Canard-Rudern gesteuerte Artillerie-Rakete - Google Patents

Mittels Canard-Rudern gesteuerte Artillerie-Rakete

Info

Publication number
DE59400761D1
DE59400761D1 DE59400761T DE59400761T DE59400761D1 DE 59400761 D1 DE59400761 D1 DE 59400761D1 DE 59400761 T DE59400761 T DE 59400761T DE 59400761 T DE59400761 T DE 59400761T DE 59400761 D1 DE59400761 D1 DE 59400761D1
Authority
DE
Germany
Prior art keywords
canard
oars
artillery missile
controlled
missile controlled
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 - Fee Related
Application number
DE59400761T
Other languages
English (en)
Inventor
Raimer Dipl Ing Steuer
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 Stiftung and Co KG
Original Assignee
Diehl GmbH and Co
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 GmbH and Co filed Critical Diehl GmbH and Co
Application granted granted Critical
Publication of DE59400761D1 publication Critical patent/DE59400761D1/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/60Steering arrangements
    • F42B10/62Steering by movement of flight surfaces
    • F42B10/64Steering by movement of flight surfaces of fins

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
DE59400761T 1993-07-28 1994-07-06 Mittels Canard-Rudern gesteuerte Artillerie-Rakete Expired - Fee Related DE59400761D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4325218A DE4325218C2 (de) 1993-07-28 1993-07-28 Artillerie-Rakete und Verfahren zur Leistungssteigerung einer Artillerie-Rakete

Publications (1)

Publication Number Publication Date
DE59400761D1 true DE59400761D1 (de) 1996-11-07

Family

ID=6493850

Family Applications (2)

Application Number Title Priority Date Filing Date
DE4325218A Expired - Fee Related DE4325218C2 (de) 1993-07-28 1993-07-28 Artillerie-Rakete und Verfahren zur Leistungssteigerung einer Artillerie-Rakete
DE59400761T Expired - Fee Related DE59400761D1 (de) 1993-07-28 1994-07-06 Mittels Canard-Rudern gesteuerte Artillerie-Rakete

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE4325218A Expired - Fee Related DE4325218C2 (de) 1993-07-28 1993-07-28 Artillerie-Rakete und Verfahren zur Leistungssteigerung einer Artillerie-Rakete

Country Status (3)

Country Link
US (1) US5467940A (de)
EP (1) EP0636852B1 (de)
DE (2) DE4325218C2 (de)

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19500993A1 (de) * 1995-01-14 1996-07-18 Contraves Gmbh Verfahren zum Bestimmen der Rollage eines rollenden Flugobjektes
DE19624187C1 (de) * 1996-06-18 1998-01-15 Diehl Gmbh & Co Rakete
DE19635847C2 (de) * 1996-09-04 1998-07-16 Daimler Benz Aerospace Ag Lenkflugkörper mit Staustrahlantrieb
US5775636A (en) * 1996-09-30 1998-07-07 The United States Of America As Represented By The Secretary Of The Army Guided artillery projectile and method
DE19645496C2 (de) * 1996-11-05 2001-05-17 Diehl Stiftung & Co Um ihre Längsachse rotierende Rakete mit Satelliten-Navigationsempfänger
US6237496B1 (en) * 1997-02-26 2001-05-29 Northrop Grumman Corporation GPS guided munition
US5943009A (en) * 1997-02-27 1999-08-24 Abbott; Anthony Steven GPS guided munition
DE19922693A1 (de) * 1999-05-18 2000-11-23 Diehl Stiftung & Co Stelleinrichtung für Ruder eines Flugkörpers
ITMI20010648A1 (it) * 2001-03-27 2002-09-27 Finmeccanica S P A Alenia Dife Gruppo di controllo per alette direzionali di missili e/o proiettili
GB0111171D0 (en) * 2001-05-08 2001-06-27 Special Cartridge Company Ltd Projictile
DE10134785A1 (de) * 2001-07-17 2003-02-06 Diehl Munitionssysteme Gmbh Verfahren zur Flugbahnkorrektur ballistisch verschossener drallstabilisierter Artilleriemunition
DE10141169A1 (de) * 2001-08-22 2003-03-13 Diehl Munitionssysteme Gmbh Artillerierakete
DE10147837A1 (de) * 2001-09-27 2003-04-24 Rheinmetall Landsysteme Gmbh Wurfsystem für einen Gefechtskopf mit einer Richtvorrichtung zur Neutralisierung von Minen
DE10236157A1 (de) 2002-08-07 2004-02-26 Junghans Feinwerktechnik Gmbh & Co. Kg Programmierbarer Artilleriezünder
US6685143B1 (en) * 2003-01-03 2004-02-03 Orbital Research Inc. Aircraft and missile forebody flow control device and method of controlling flow
US7121210B2 (en) * 2003-02-18 2006-10-17 Kdi Precision Products, Inc. Accuracy fuze for airburst cargo delivery projectiles
WO2005026654A2 (en) 2003-05-08 2005-03-24 Incucomm, Inc. Weapon and weapon system employing the same
US7530315B2 (en) 2003-05-08 2009-05-12 Lone Star Ip Holdings, Lp Weapon and weapon system employing the same
IL162027A (en) * 2004-05-17 2009-05-04 Rafael Advanced Defense Sys Method and system for resetting the flight path of a non-guided bullet, including compensation for deviation from the oscillations of the launcher
US7834300B2 (en) * 2005-02-07 2010-11-16 Bae Systems Information And Electronic Systems Integration Inc. Ballistic guidance control for munitions
US7503521B2 (en) * 2005-02-07 2009-03-17 Bae Systems Information And Electronic Systems Integration Inc. Radiation homing tag
US8450668B2 (en) * 2005-02-07 2013-05-28 Bae Systems Information And Electronic Systems Integration Inc. Optically guided munition control system and method
WO2006088687A1 (en) * 2005-02-07 2006-08-24 Bae Systems Information And Electronic Systems Integration Inc. Optically guided munition
WO2006086532A2 (en) * 2005-02-07 2006-08-17 Bae Systems Information And Electronic Systems Three axis aerodynamic control of guided munitions
US7895946B2 (en) 2005-09-30 2011-03-01 Lone Star Ip Holdings, Lp Small smart weapon and weapon system employing the same
US7690304B2 (en) * 2005-09-30 2010-04-06 Lone Star Ip Holdings, Lp Small smart weapon and weapon system employing the same
US8541724B2 (en) 2006-09-29 2013-09-24 Lone Star Ip Holdings, Lp Small smart weapon and weapon system employing the same
IL178840A0 (en) * 2006-10-24 2007-09-20 Rafael Advanced Defense Sys System
US8117955B2 (en) 2006-10-26 2012-02-21 Lone Star Ip Holdings, Lp Weapon interface system and delivery platform employing the same
US7926402B2 (en) * 2006-11-29 2011-04-19 Alliant Techsystems Inc. Method and apparatus for munition timing and munitions incorporating same
US8546736B2 (en) 2007-03-15 2013-10-01 Raytheon Company Modular guided projectile
US7947938B2 (en) * 2007-03-15 2011-05-24 Raytheon Company Methods and apparatus for projectile guidance
US7791007B2 (en) * 2007-06-21 2010-09-07 Woodward Hrt, Inc. Techniques for providing surface control to a guidable projectile
SE534614C2 (sv) * 2010-02-25 2011-10-25 Bae Systems Bofors Ab Granat anordnad med utfällbara vingar och styranordning
US8933383B2 (en) * 2010-09-01 2015-01-13 The United States Of America As Represented By The Secretary Of The Army Method and apparatus for correcting the trajectory of a fin-stabilized, ballistic projectile using canards
US9068803B2 (en) 2011-04-19 2015-06-30 Lone Star Ip Holdings, Lp Weapon and weapon system employing the same

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3067681A (en) * 1960-01-04 1962-12-11 Telecomputing Corp Guided missile
US3272124A (en) * 1960-11-28 1966-09-13 Pneumo Dynamics Corp Solid propellant actuation system
FR1528934A (fr) * 1966-06-21 1968-06-14 Gen Dynamics Corp Dispositif de commande perfectionné pour engins volants, notamment pour missiles
US4438893A (en) * 1973-08-10 1984-03-27 Sanders Associates, Inc. Prime power source and control for a guided projectile
DE2853779B2 (de) * 1978-12-13 1981-07-16 Diehl GmbH & Co, 8500 Nürnberg Rollagemesser für drallstabilisierte Flugkörper und Geschosse
DE3013405C2 (de) * 1980-04-05 1983-10-20 GRS Gesellschaft für Raketen-Systeme mbH, 5300 Bonn Verfahren zum Vermeiden des Nachrichtens von Abschußgeräten für ballistische Flugkörper
US4394997A (en) * 1980-04-14 1983-07-26 General Dynamics, Pomona Division Sequential time discrimination system for sub-delivery systems
US4530476A (en) * 1981-08-12 1985-07-23 E-Systems, Inc. Ordnance delivery system and method including remotely piloted or programmable aircraft with yaw-to-turn guidance system
US4606514A (en) * 1984-08-10 1986-08-19 Martin-Marietta Corporation Method for homing a projectile onto a target and for determining the ballistic trajectory thereof as well as arrangements for implementing the method
US4662580A (en) * 1985-06-20 1987-05-05 The United States Of America As Represented By The Secretary Of The Navy Simple diver reentry method
GB2184414B (en) * 1985-12-21 1989-10-18 Plessey Co Plc Rocket propelled vehicle
DE3645093C2 (en) * 1986-02-27 1991-06-13 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De Flying body steering system with connected motor
GB8612440D0 (en) * 1986-05-22 1986-09-17 Short Brothers Plc Unmanned flight body
DE3707159A1 (de) * 1987-03-06 1988-09-15 Diehl Gmbh & Co Vorrichtung zum autonomen bestimmen des nickwinkels an bord eines projektils
DE3716606A1 (de) * 1987-05-18 1988-12-08 Diehl Gmbh & Co Verfahren und einrichtung zum bestimmen des apogaeums-durchganges
FR2622966B1 (fr) * 1987-11-06 1993-05-07 Thomson Brandt Armements Dispositif de stabilisation gyroscopique pour un organe de manoeuvre de projectile
DE3738580A1 (de) * 1987-11-13 1989-06-01 Diehl Gmbh & Co Gelenktes artillerieprojektil mit flugbahnregler
KR910010183B1 (ko) * 1988-12-22 1991-12-20 삼성전자 주식회사 녹화 정지 시간 설정 방법
DE3904684A1 (de) * 1989-02-16 1990-09-20 Asea Brown Boveri Verfahren zur korrektur der flugbahn aus einer rohrwaffe abgefeuerten oder selbststangetriebenen explosivgeschosses sowie geschoss, auf das das verfahren angewendet wird
DE4120367A1 (de) * 1991-06-20 1992-12-24 Diehl Gmbh & Co Einrichtung zur messung des hoehenprofils eines bodenwindes
US5260709A (en) * 1991-12-19 1993-11-09 Hughes Aircraft Company Autonomous precision weapon delivery using synthetic array radar
US5322243A (en) * 1992-06-25 1994-06-21 Northrop Corporation Separately banking maneuvering aerodynamic control surfaces, system and method

Also Published As

Publication number Publication date
DE4325218A1 (de) 1995-02-02
EP0636852B1 (de) 1996-10-02
US5467940A (en) 1995-11-21
DE4325218C2 (de) 1998-10-22
EP0636852A1 (de) 1995-02-01

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: DIEHL STIFTUNG & CO., 90478 NUERNBERG, DE

8339 Ceased/non-payment of the annual fee