DE2141744C3 - Flugkörper mit Schubvektor- und aerodynamischer Steuerung - Google Patents

Flugkörper mit Schubvektor- und aerodynamischer Steuerung

Info

Publication number
DE2141744C3
DE2141744C3 DE2141744A DE2141744A DE2141744C3 DE 2141744 C3 DE2141744 C3 DE 2141744C3 DE 2141744 A DE2141744 A DE 2141744A DE 2141744 A DE2141744 A DE 2141744A DE 2141744 C3 DE2141744 C3 DE 2141744C3
Authority
DE
Germany
Prior art keywords
missile
jet
aerodynamic
thrust vector
flaps
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
DE2141744A
Other languages
German (de)
English (en)
Other versions
DE2141744A1 (de
DE2141744B2 (de
Inventor
Dieter Dipl.-Ing. 8014 Neubiberg Weis
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Priority to DE2141744A priority Critical patent/DE2141744C3/de
Priority to US00275970A priority patent/US3776490A/en
Priority to FR7228973A priority patent/FR2150342A1/fr
Publication of DE2141744A1 publication Critical patent/DE2141744A1/de
Publication of DE2141744B2 publication Critical patent/DE2141744B2/de
Application granted granted Critical
Publication of DE2141744C3 publication Critical patent/DE2141744C3/de
Expired 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
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/665—Steering by varying intensity or direction of thrust characterised by using a nozzle provided with at least a deflector mounted within the nozzle
    • 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
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins

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)
DE2141744A 1971-08-20 1971-08-20 Flugkörper mit Schubvektor- und aerodynamischer Steuerung Expired DE2141744C3 (de)

Priority Applications (3)

Application Number Priority Date Filing Date Title
DE2141744A DE2141744C3 (de) 1971-08-20 1971-08-20 Flugkörper mit Schubvektor- und aerodynamischer Steuerung
US00275970A US3776490A (en) 1971-08-20 1972-07-28 Missile with thrust vector and aerodynamic control
FR7228973A FR2150342A1 (enExample) 1971-08-20 1972-08-10

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2141744A DE2141744C3 (de) 1971-08-20 1971-08-20 Flugkörper mit Schubvektor- und aerodynamischer Steuerung

Publications (3)

Publication Number Publication Date
DE2141744A1 DE2141744A1 (de) 1973-03-01
DE2141744B2 DE2141744B2 (de) 1978-01-19
DE2141744C3 true DE2141744C3 (de) 1978-09-14

Family

ID=5817280

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2141744A Expired DE2141744C3 (de) 1971-08-20 1971-08-20 Flugkörper mit Schubvektor- und aerodynamischer Steuerung

Country Status (3)

Country Link
US (1) US3776490A (enExample)
DE (1) DE2141744C3 (enExample)
FR (1) FR2150342A1 (enExample)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4198016A (en) * 1978-06-12 1980-04-15 The United States Of America As Represented By The Secretary Of The Navy Floating canard with geared tab
US4274610A (en) * 1978-07-14 1981-06-23 General Dynamics, Pomona Division Jet tab control mechanism for thrust vector control
US4364531A (en) * 1980-10-09 1982-12-21 Knoski Jerry L Attachable airfoil with movable control surface
GB8611406D0 (en) * 1986-05-09 1986-08-20 Lucas Ind Plc Missile flight control system
US4867393A (en) * 1988-08-17 1989-09-19 Morton Thiokol, Inc. Reduced fin span thrust vector controlled pulsed tactical missile
US5873549A (en) * 1996-09-25 1999-02-23 Mcdonnell Douglas Corporation Vehicle rotation and control mechanism
FR2799833B1 (fr) * 1999-10-15 2002-10-25 Tda Armements Sas Dispositif de correction de trajectoire pour projectiles guides gyroscopes
US6502785B1 (en) * 1999-11-17 2003-01-07 Lockheed Martin Corporation Three axis flap control system
FR2839360B1 (fr) * 2002-05-02 2006-05-19 Sagem Procede de controle de la trajectoire d'un objet largable, objet largable et module stabilisateur avant pour objet largable
USD599854S1 (en) * 2008-06-09 2009-09-08 Lockheed Martin Corporation Writing instrument

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2968454A (en) * 1951-10-29 1961-01-17 Martin Co Rocket control system
US3139033A (en) * 1959-07-23 1964-06-30 Ernst D Geissler Aerodynamically stable missile
US3305194A (en) * 1960-03-08 1967-02-21 Robert G Conard Wind-insensitive missile
GB1188651A (en) * 1962-03-05 1970-04-22 British Aircraft Corp Ltd Improvements in or relating to Missiles
US3188958A (en) * 1963-03-11 1965-06-15 James D Burke Range control for a ballistic missile

Also Published As

Publication number Publication date
DE2141744A1 (de) 1973-03-01
DE2141744B2 (de) 1978-01-19
FR2150342A1 (enExample) 1973-04-06
US3776490A (en) 1973-12-04

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Legal Events

Date Code Title Description
C3 Grant after two publication steps (3rd publication)
EF Willingness to grant licences
8339 Ceased/non-payment of the annual fee