EP1635135A1 - Tête de missile et procédé de guidage de missile - Google Patents

Tête de missile et procédé de guidage de missile Download PDF

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Publication number
EP1635135A1
EP1635135A1 EP05019036A EP05019036A EP1635135A1 EP 1635135 A1 EP1635135 A1 EP 1635135A1 EP 05019036 A EP05019036 A EP 05019036A EP 05019036 A EP05019036 A EP 05019036A EP 1635135 A1 EP1635135 A1 EP 1635135A1
Authority
EP
European Patent Office
Prior art keywords
head
missile
head tip
tip
intersection
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.)
Withdrawn
Application number
EP05019036A
Other languages
German (de)
English (en)
Inventor
Willi Ruggaber
Hans Kordulla
Wilhelm Hinding
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 EP1635135A1 publication Critical patent/EP1635135A1/fr
Withdrawn legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B19/00—Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means
    • F42B19/01—Steering control
    • 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
    • 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
    • F42B10/38—Range-increasing arrangements
    • F42B10/42—Streamlined projectiles
    • F42B10/46—Streamlined nose cones; Windshields; Radomes

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
EP05019036A 2004-09-10 2005-09-01 Tête de missile et procédé de guidage de missile Withdrawn EP1635135A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102004043758A DE102004043758A1 (de) 2004-09-10 2004-09-10 Flugkörperkopf und Verfahren zur Lenkung eines Flugkörpers

Publications (1)

Publication Number Publication Date
EP1635135A1 true EP1635135A1 (fr) 2006-03-15

Family

ID=35458214

Family Applications (1)

Application Number Title Priority Date Filing Date
EP05019036A Withdrawn EP1635135A1 (fr) 2004-09-10 2005-09-01 Tête de missile et procédé de guidage de missile

Country Status (3)

Country Link
EP (1) EP1635135A1 (fr)
DE (1) DE102004043758A1 (fr)
SG (1) SG121091A1 (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008118159A3 (fr) * 2006-12-14 2008-12-11 Simmonds Precision Products Commande de trajectoire de projectile gyro-stabilisatrice
WO2009009193A2 (fr) 2007-06-21 2009-01-15 Hr Textron Inc. Techniques permettant de fournir une commande de surface à un projectile guidable
WO2009011949A2 (fr) 2007-06-12 2009-01-22 Hr Textron Inc. Techniques d'articulation du nez d'un projectile guidable
CN113772124A (zh) * 2021-10-15 2021-12-10 中国工程物理研究院总体工程研究所 一种稠密大气中高速飞行回转体用全包两级对开分离舱
CN114963889A (zh) * 2022-06-14 2022-08-30 西北工业大学 一种潜射式跨域跨介质导弹

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113280690B (zh) * 2021-04-29 2022-10-21 北京临近空间飞行器系统工程研究所 一种采用柔性蒙皮的双伺服驱动端头摆动结构及控制方法

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2594766A (en) * 1946-11-30 1952-04-29 Esther C Goddard Apparatus for steering aircraft
US4579298A (en) * 1981-04-08 1986-04-01 The Commonwealth Of Australia Directional control device for airborne or seaborne missiles
DE3628152C1 (de) * 1986-08-19 1987-09-10 Messerschmitt Boelkow Blohm Flugkoerper mit aerodynamischer Steuerung
US6467722B1 (en) * 2002-01-31 2002-10-22 The United States Of America As Represented By The Secretary Of The Army Magnetostrictive missile guidance system

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3069112A (en) * 1956-08-20 1962-12-18 Raymond T Patterson Radome
US3262655A (en) * 1963-12-26 1966-07-26 Jr Warren Gillespie Alleviation of divergence during rocket launch
DE3503041C1 (de) * 1985-01-30 1986-09-11 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Schnellfliegender Flugkörper mit aerodynamischer Steuerung
DE3815290C1 (fr) * 1988-05-05 1989-08-17 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2594766A (en) * 1946-11-30 1952-04-29 Esther C Goddard Apparatus for steering aircraft
US4579298A (en) * 1981-04-08 1986-04-01 The Commonwealth Of Australia Directional control device for airborne or seaborne missiles
DE3628152C1 (de) * 1986-08-19 1987-09-10 Messerschmitt Boelkow Blohm Flugkoerper mit aerodynamischer Steuerung
US6467722B1 (en) * 2002-01-31 2002-10-22 The United States Of America As Represented By The Secretary Of The Army Magnetostrictive missile guidance system

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008118159A3 (fr) * 2006-12-14 2008-12-11 Simmonds Precision Products Commande de trajectoire de projectile gyro-stabilisatrice
US7963442B2 (en) 2006-12-14 2011-06-21 Simmonds Precision Products, Inc. Spin stabilized projectile trajectory control
WO2009011949A2 (fr) 2007-06-12 2009-01-22 Hr Textron Inc. Techniques d'articulation du nez d'un projectile guidable
WO2009011949A3 (fr) * 2007-06-12 2009-05-14 Hr Textron Inc Techniques d'articulation du nez d'un projectile guidable
US7696459B2 (en) 2007-06-12 2010-04-13 Hr Textron, Inc. Techniques for articulating a nose member of a guidable projectile
WO2009009193A2 (fr) 2007-06-21 2009-01-15 Hr Textron Inc. Techniques permettant de fournir une commande de surface à un projectile guidable
WO2009009193A3 (fr) * 2007-06-21 2009-05-07 Hr Textron Inc Techniques permettant de fournir une commande de surface à un projectile guidable
US7791007B2 (en) 2007-06-21 2010-09-07 Woodward Hrt, Inc. Techniques for providing surface control to a guidable projectile
CN113772124A (zh) * 2021-10-15 2021-12-10 中国工程物理研究院总体工程研究所 一种稠密大气中高速飞行回转体用全包两级对开分离舱
CN114963889A (zh) * 2022-06-14 2022-08-30 西北工业大学 一种潜射式跨域跨介质导弹

Also Published As

Publication number Publication date
SG121091A1 (en) 2006-04-26
DE102004043758A1 (de) 2006-03-30

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