SG121091A1 - Missile nose and method for steering a missile - Google Patents

Missile nose and method for steering a missile

Info

Publication number
SG121091A1
SG121091A1 SG200505582A SG200505582A SG121091A1 SG 121091 A1 SG121091 A1 SG 121091A1 SG 200505582 A SG200505582 A SG 200505582A SG 200505582 A SG200505582 A SG 200505582A SG 121091 A1 SG121091 A1 SG 121091A1
Authority
SG
Singapore
Prior art keywords
missile
steering
nose
missile nose
Prior art date
Application number
SG200505582A
Other languages
English (en)
Inventor
Willi Ruggaber
Hans Kordulla
Wilhelm Hinding
Original Assignee
Diehl Bgt Defence Gmbh & 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 & Co Kg filed Critical Diehl Bgt Defence Gmbh & Co Kg
Publication of SG121091A1 publication Critical patent/SG121091A1/en

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)
SG200505582A 2004-09-10 2005-08-31 Missile nose and method for steering a missile SG121091A1 (en)

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
SG121091A1 true SG121091A1 (en) 2006-04-26

Family

ID=35458214

Family Applications (1)

Application Number Title Priority Date Filing Date
SG200505582A SG121091A1 (en) 2004-09-10 2005-08-31 Missile nose and method for steering a missile

Country Status (3)

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

Families Citing this family (6)

* 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
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
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

Family Cites Families (8)

* 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
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
WO1982003453A1 (fr) * 1981-04-08 1982-10-14 Thomson Keith Donald 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
DE3628152C1 (de) * 1986-08-19 1987-09-10 Messerschmitt Boelkow Blohm Flugkoerper mit aerodynamischer Steuerung
DE3815290C1 (fr) * 1988-05-05 1989-08-17 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
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

Also Published As

Publication number Publication date
EP1635135A1 (fr) 2006-03-15
DE102004043758A1 (de) 2006-03-30

Similar Documents

Publication Publication Date Title
EP1743239A4 (fr) Procede et systeme de reconnaissance de caracteres
EP2074572A4 (fr) Système et procédé pour fournir une marque pour un véhicule d'occasion
EG23824A (en) System and method for communicating along a wellbore
EP1838566A4 (fr) Procede et appareil de commande de direction
EP1947966A4 (fr) Système et procédé de protection d une partie du corps
TWI368154B (en) System and method for selecting a view mode and setting
GB0524719D0 (en) A vehicle control system and method
IL183001A0 (en) Missile control system and method
IL179971A0 (en) An inhalation device and a method for assembling said inhalation device
EP1734334A4 (fr) Procede d'explosion
EP1865661A4 (fr) Procédé de multidiffusion rapide et système idoine
ZA200704386B (en) Method for increasing a ethaboxam effectiveness
EP1722920A4 (fr) Systeme et procede de commande d'un percuteur
EP1707914A4 (fr) Procede de traitement par explosion
SG121091A1 (en) Missile nose and method for steering a missile
ZA200701276B (en) A system and a method for mission planning
ZA200708734B (en) Steering system and method for a guided flying apparatus
EP1827876A4 (fr) Procédé et disposition pour accroître la sécurité quand on manipule une roue
GB0612097D0 (en) A Compliance facilitating system and method
GB0402317D0 (en) A tracking system and method
TWI350537B (en) Closed-loop servo system and servo method
IL178933A0 (en) Method and system for creating a manual
GB0422378D0 (en) A method
EP2033151A4 (fr) Procede et systeme
IL179304A0 (en) A method and system for debriefing flying scenes