EP0180722A3 - Missile - Google Patents

Missile Download PDF

Info

Publication number
EP0180722A3
EP0180722A3 EP85109643A EP85109643A EP0180722A3 EP 0180722 A3 EP0180722 A3 EP 0180722A3 EP 85109643 A EP85109643 A EP 85109643A EP 85109643 A EP85109643 A EP 85109643A EP 0180722 A3 EP0180722 A3 EP 0180722A3
Authority
EP
European Patent Office
Prior art keywords
missile
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
EP85109643A
Other languages
German (de)
Other versions
EP0180722A2 (en
EP0180722B1 (en
Inventor
Klaus Unterstein
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.)
Rheinmetall Industrie AG
Original Assignee
Rheinmetall GmbH
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 Rheinmetall GmbH filed Critical Rheinmetall GmbH
Publication of EP0180722A2 publication Critical patent/EP0180722A2/en
Publication of EP0180722A3 publication Critical patent/EP0180722A3/en
Application granted granted Critical
Publication of EP0180722B1 publication Critical patent/EP0180722B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/20—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel deployed by combustion gas pressure, or by pneumatic or hydraulic forces

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
EP19850109643 1984-09-05 1985-07-31 Missile Expired - Lifetime EP0180722B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3432614 1984-09-05
DE19843432614 DE3432614A1 (en) 1984-09-05 1984-09-05 MISSILE

Publications (3)

Publication Number Publication Date
EP0180722A2 EP0180722A2 (en) 1986-05-14
EP0180722A3 true EP0180722A3 (en) 1990-03-21
EP0180722B1 EP0180722B1 (en) 1992-06-03

Family

ID=6244693

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19850109643 Expired - Lifetime EP0180722B1 (en) 1984-09-05 1985-07-31 Missile

Country Status (4)

Country Link
US (1) US4659037A (en)
EP (1) EP0180722B1 (en)
DE (2) DE3432614A1 (en)
ES (1) ES8801027A1 (en)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3507677A1 (en) * 1985-03-05 1986-09-11 Diehl GmbH & Co, 8500 Nürnberg MISSILE WITH OVER-CALIBRATE ANALYSIS
FR2812936A1 (en) * 1986-08-12 2002-02-15 Aerospatiale Missile with variable wing configuration has moving wings extending from slots in hollow fixed wings on missile body
DE3721512C1 (en) * 1987-06-30 1989-03-30 Diehl Gmbh & Co Missile with over-caliber tail unit
DE3918244A1 (en) * 1989-06-05 1990-12-06 Diehl Gmbh & Co FOLDING WING FROM A MISSILE
US5120947A (en) * 1990-03-29 1992-06-09 International Totalizator Systems, Inc. Apparatus and method for processing a ticket
DE4020897C2 (en) * 1990-06-30 1993-11-11 Diehl Gmbh & Co Device for unlocking and swinging out the rudder blades of a projectile
DE4105142A1 (en) * 1991-02-20 1992-08-27 Diehl Gmbh & Co PROJECTILE WITH FOLD-OUT PAD
US5211358A (en) * 1991-05-13 1993-05-18 General Dynamics Corporation Airfoil deployment system for missile or aircraft
US6073880A (en) * 1998-05-18 2000-06-13 Versatron, Inc. Integrated missile fin deployment system
US6186443B1 (en) 1998-06-25 2001-02-13 International Dynamics Corporation Airborne vehicle having deployable wing and control surface
DE10162136B4 (en) * 2001-12-18 2004-10-14 Diehl Munitionssysteme Gmbh & Co. Kg Missile to be fired from a tube with an over-caliber tail unit
DE10205043C5 (en) 2002-02-07 2010-06-17 Diehl Bgt Defence Gmbh & Co. Kg From a tube to be closed missile with überkalibrigem tail
US7800031B2 (en) * 2005-09-07 2010-09-21 Omnitek Partners Llc Actuators for gun-fired projectiles and mortars
FR2909972B1 (en) * 2006-12-18 2009-10-23 Novadem Sarl VERTICAL TAKE-OFF AIRCRAFT
FR2952712A1 (en) 2009-11-16 2011-05-20 Nexter Munitions PROJECTILE BODY EQUIPPED WITH DEPLOYABLE APPENDICES
CN103522248B (en) * 2013-10-11 2015-08-05 北京航天新风机械设备有限责任公司 A kind of special tooling folding for rudder/aerofoil
EP3318490B1 (en) * 2016-11-03 2019-06-12 Diehl Defence GmbH & Co. KG Method for ejecting a missile
IL250433B (en) * 2017-02-02 2021-01-31 Israel Aerospace Ind Ltd Apparatus for a vehicle
US11300390B1 (en) 2018-03-05 2022-04-12 Dynamic Structures And Materials, Llc Control surface deployment apparatus and method of use
CN112525016A (en) * 2020-12-22 2021-03-19 湖北航天化学技术研究所 Gas generating device and driving device
CN113899265A (en) * 2021-10-12 2022-01-07 西安现代控制技术研究所 Folding rudder wing opening time measuring device based on photoelectric element

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3047257A (en) * 1958-04-24 1962-07-31 Martin Marietta Corp Device for changing airfoil profile
US3633846A (en) * 1970-05-28 1972-01-11 Us Navy Expandable aerodynamic fin
DE2518593C3 (en) * 1975-04-26 1979-12-06 Diehl Gmbh & Co, 8500 Nuernberg Mortar projectile
US4262862A (en) * 1978-02-18 1981-04-21 Messerschmitt-Bolkow-Blohm Gesellschaft mit beschraankter Haftung Apparatus for changing the wing positions of swingable wings of a missile
DE2342783C2 (en) * 1973-08-24 1983-12-22 Rheinmetall GmbH, 4000 Düsseldorf Projectile equipped with a tail unit

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE428969B (en) * 1977-02-09 1983-08-01 Bofors Ab DEVICE FOR FENSTABILIZED GRANATE
US4143838A (en) * 1977-08-22 1979-03-13 The United States Of America As Represented By The Secretary Of The Navy Folding fin assembly detent
US4203569A (en) * 1977-10-17 1980-05-20 Bei Electronics, Inc. Fin and nozzle unit for a free-flight rocket
US4364531A (en) * 1980-10-09 1982-12-21 Knoski Jerry L Attachable airfoil with movable control surface
US4478150A (en) * 1983-01-12 1984-10-23 The United States Of America As Represented By The Secretary Of The Army Cartridge with elastic pusher cup
US4586681A (en) * 1983-06-27 1986-05-06 General Dynamics Pomona Division Supersonic erectable fabric wings

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3047257A (en) * 1958-04-24 1962-07-31 Martin Marietta Corp Device for changing airfoil profile
US3633846A (en) * 1970-05-28 1972-01-11 Us Navy Expandable aerodynamic fin
DE2342783C2 (en) * 1973-08-24 1983-12-22 Rheinmetall GmbH, 4000 Düsseldorf Projectile equipped with a tail unit
DE2518593C3 (en) * 1975-04-26 1979-12-06 Diehl Gmbh & Co, 8500 Nuernberg Mortar projectile
US4262862A (en) * 1978-02-18 1981-04-21 Messerschmitt-Bolkow-Blohm Gesellschaft mit beschraankter Haftung Apparatus for changing the wing positions of swingable wings of a missile

Also Published As

Publication number Publication date
EP0180722A2 (en) 1986-05-14
US4659037A (en) 1987-04-21
ES546443A0 (en) 1987-12-16
ES8801027A1 (en) 1987-12-16
DE3432614A1 (en) 1986-03-13
EP0180722B1 (en) 1992-06-03
DE3586163D1 (en) 1992-07-09

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