ATE373808T1 - Querschub-steuervorrichtung - Google Patents

Querschub-steuervorrichtung

Info

Publication number
ATE373808T1
ATE373808T1 AT04023729T AT04023729T ATE373808T1 AT E373808 T1 ATE373808 T1 AT E373808T1 AT 04023729 T AT04023729 T AT 04023729T AT 04023729 T AT04023729 T AT 04023729T AT E373808 T1 ATE373808 T1 AT E373808T1
Authority
AT
Austria
Prior art keywords
control device
thrust control
transverse thrust
propellant
cable
Prior art date
Application number
AT04023729T
Other languages
English (en)
Inventor
Thomas Heitmann
Michael Schwenzer
Original Assignee
Rheinmetall Waffe Munition
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 Waffe Munition filed Critical Rheinmetall Waffe Munition
Application granted granted Critical
Publication of ATE373808T1 publication Critical patent/ATE373808T1/de

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
    • 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
    • F42B10/661—Steering by varying intensity or direction of thrust using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Air Bags (AREA)
  • Transmission Devices (AREA)
  • Elimination Of Static Electricity (AREA)
  • Vehicle Body Suspensions (AREA)
  • Plasma Technology (AREA)
  • Installation Of Indoor Wiring (AREA)
AT04023729T 2003-11-19 2004-10-05 Querschub-steuervorrichtung ATE373808T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE10354098A DE10354098A1 (de) 2003-11-19 2003-11-19 Querschub-Steuervorrichtung

Publications (1)

Publication Number Publication Date
ATE373808T1 true ATE373808T1 (de) 2007-10-15

Family

ID=34428805

Family Applications (1)

Application Number Title Priority Date Filing Date
AT04023729T ATE373808T1 (de) 2003-11-19 2004-10-05 Querschub-steuervorrichtung

Country Status (5)

Country Link
US (1) US7118065B1 (de)
EP (1) EP1533589B1 (de)
AT (1) ATE373808T1 (de)
DE (2) DE10354098A1 (de)
ES (1) ES2290601T3 (de)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7416154B2 (en) * 2005-09-16 2008-08-26 The United States Of America As Represented By The Secretary Of The Army Trajectory correction kit
US7875838B1 (en) * 2007-04-04 2011-01-25 The United States Of America As Represented By The Secretary Of The Navy Post boost control power assembly
US8362408B2 (en) * 2009-10-22 2013-01-29 Honeywell International Inc. Steerable projectile charging system
US20140137539A1 (en) * 2012-11-19 2014-05-22 Raytheon Company Thrust-producing device with detonation motor
US9068808B2 (en) * 2013-01-17 2015-06-30 Raytheon Company Air vehicle with bilateral steering thrusters
US10914559B1 (en) * 2016-11-21 2021-02-09 Lockheed Martin Corporation Missile, slot thrust attitude controller system, and method

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3034434A (en) * 1960-03-08 1962-05-15 Frank H Swaim Thrust vector control system
US3868883A (en) * 1964-02-20 1975-03-04 Mc Donnell Douglas Corp Guidance system
US3860199A (en) * 1972-01-03 1975-01-14 Ship Systems Inc Laser-guided projectile system
DE4036166A1 (de) * 1990-11-14 1992-05-21 Diehl Gmbh & Co Bahnkorrigierbares projektil
DE4408085C2 (de) * 1994-03-10 1999-08-12 Rheinmetall W & M Gmbh Vorrichtung zur Lenkung eines nicht um seine Längsachse rotierenden Flugkörpers
DE4410326C2 (de) * 1994-03-25 1998-07-02 Rheinmetall Ind Ag Geschoß mit einer Vorrichtung zur Flugbahnkorrektur
US6367735B1 (en) * 2000-02-10 2002-04-09 Quantic Industries, Inc. Projectile diverter
DE10141169A1 (de) * 2001-08-22 2003-03-13 Diehl Munitionssysteme Gmbh Artillerierakete

Also Published As

Publication number Publication date
ES2290601T3 (es) 2008-02-16
DE10354098A1 (de) 2005-06-23
EP1533589A1 (de) 2005-05-25
EP1533589B1 (de) 2007-09-19
US7118065B1 (en) 2006-10-10
DE502004005009D1 (de) 2007-10-31

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