DE102004043758A1 - Flugkörperkopf und Verfahren zur Lenkung eines Flugkörpers - Google Patents

Flugkörperkopf und Verfahren zur Lenkung eines Flugkörpers Download PDF

Info

Publication number
DE102004043758A1
DE102004043758A1 DE102004043758A DE102004043758A DE102004043758A1 DE 102004043758 A1 DE102004043758 A1 DE 102004043758A1 DE 102004043758 A DE102004043758 A DE 102004043758A DE 102004043758 A DE102004043758 A DE 102004043758A DE 102004043758 A1 DE102004043758 A1 DE 102004043758A1
Authority
DE
Germany
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.)
Ceased
Application number
DE102004043758A
Other languages
German (de)
English (en)
Inventor
Willi Dipl.-Ing. Ruggaber
Hans Dipl.-Ing. Kordulla
Wilhelm Dipl.-Ing. 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
Priority to DE102004043758A priority Critical patent/DE102004043758A1/de
Priority to SG200505582A priority patent/SG121091A1/en
Priority to EP05019036A priority patent/EP1635135A1/fr
Publication of DE102004043758A1 publication Critical patent/DE102004043758A1/de
Ceased 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
    • 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)
DE102004043758A 2004-09-10 2004-09-10 Flugkörperkopf und Verfahren zur Lenkung eines Flugkörpers Ceased DE102004043758A1 (de)

Priority Applications (3)

Application Number Priority Date Filing Date Title
DE102004043758A DE102004043758A1 (de) 2004-09-10 2004-09-10 Flugkörperkopf und Verfahren zur Lenkung eines Flugkörpers
SG200505582A SG121091A1 (en) 2004-09-10 2005-08-31 Missile nose and method for steering a missile
EP05019036A EP1635135A1 (fr) 2004-09-10 2005-09-01 Tête de missile et procédé de guidage de missile

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
DE102004043758A1 true DE102004043758A1 (de) 2006-03-30

Family

ID=35458214

Family Applications (1)

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

Country Status (3)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113280690A (zh) * 2021-04-29 2021-08-20 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

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7963442B2 (en) * 2006-12-14 2011-06-21 Simmonds Precision Products, Inc. Spin stabilized projectile trajectory control
US7696459B2 (en) 2007-06-12 2010-04-13 Hr Textron, Inc. Techniques for articulating a nose member of a guidable projectile
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

Citations (5)

* 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
EP0076271B1 (fr) * 1981-04-08 1985-11-21 The Commonwealth Of Australia Dispositif de commande directionnelle pour missiles se deplacant dans l'air ou dans l'eau
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

Family Cites Families (3)

* 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
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

Patent Citations (5)

* 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
EP0076271B1 (fr) * 1981-04-08 1985-11-21 The Commonwealth Of Australia Dispositif de commande directionnelle pour missiles se deplacant dans l'air ou dans l'eau
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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113280690A (zh) * 2021-04-29 2021-08-20 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

Also Published As

Publication number Publication date
SG121091A1 (en) 2006-04-26
EP1635135A1 (fr) 2006-03-15

Similar Documents

Publication Publication Date Title
EP2876041B1 (fr) Agencement de détermination d'une force agissant sur un gouvernail
EP1813907B1 (fr) Corps volant pour le domaine supersonique
EP0238717B1 (fr) Missile dirigible
EP1635135A1 (fr) Tête de missile et procédé de guidage de missile
DE2410255C2 (de) Kreuzrudersystem für eine Rakete
DE4306913A1 (de) Feuerleiteinrichtung für, insbesondere mobile, Flugabwehrsysteme
DE602005000222T2 (de) Flugkörper zur Geländeaufklärung
DE60200899T2 (de) Steuerungsgruppe für die Steuerungsflossen von Raketen oder Geschossen
DE19949640A1 (de) Verfahren und Vorrichtung zum schnellen Umwenden eines Bewegungskörpers in einem fluiden Medium
DE2445938A1 (de) Schleppkoerper zur darstellung von luftzielen
EP3738876B1 (fr) Missile de croisière et procédé de commande d'un missile de croisière
DE1087909B (de) Ruderanlage fuer Flugkoerper mit einer Brennkammer fuer einen festen Treibsatz
DE1153657B (de) Antriebs- und Steuervorrichtung fuer die Endstufe einer mehrstufigen Traegerrakete
DE102014010109A1 (de) Flugkörper
DE2037819A1 (de) Richtvorrichtung
DE2141628C3 (de) Schwerkraftgesteuerte Stabilisierungsflosse für Unterwasserkörper
DE2813032C1 (de) Gleitgeschoss
DE1781098B2 (de) Lenkregelkreis
DE1141537B (de) Stabilisierungsanordnung fuer ferngelenkte unbemannte Flugkoerper
EP2876405B1 (fr) Missile guidé et procédé de guidage d'un missile guidé
DE102023103889B3 (de) Sichere Führung eines Kabels an einem Unterseeboot
DE102012020740B4 (de) Verfahren zum Umrüsten einer Munition für eine schulterstützbare Waffe
DE102016200468A1 (de) Durchstoßvorrichtung zum Durchstoßen einer Wandstruktur
EP1108645A2 (fr) Dispositif pour gouverner des embarcations
DE3726241A1 (de) Strahllenkersystem fuer wasserstrahlantrieb

Legal Events

Date Code Title Description
OP8 Request for examination as to paragraph 44 patent law
8122 Nonbinding interest in granting licences declared
8131 Rejection