EP0384965A3 - Flügelstabilisierter Submunitionskörper - Google Patents

Flügelstabilisierter Submunitionskörper Download PDF

Info

Publication number
EP0384965A3
EP0384965A3 EP19890120959 EP89120959A EP0384965A3 EP 0384965 A3 EP0384965 A3 EP 0384965A3 EP 19890120959 EP19890120959 EP 19890120959 EP 89120959 A EP89120959 A EP 89120959A EP 0384965 A3 EP0384965 A3 EP 0384965A3
Authority
EP
European Patent Office
Prior art keywords
stabilized
subprojectile
fin
submunition
submunitions
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Withdrawn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
EP19890120959
Other languages
English (en)
French (fr)
Other versions
EP0384965A2 (de
Inventor
Gerhard Dr. Glotz
Werner Grosswendt
Helmut Dr. Peller
Jens Dr. Seidensticker
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.)
Rheinmetall Industrie AG
Original Assignee
Rheinmetall GmbH
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 GmbH filed Critical Rheinmetall GmbH
Publication of EP0384965A2 publication Critical patent/EP0384965A2/de
Publication of EP0384965A3 publication Critical patent/EP0384965A3/de
Withdrawn legal-status Critical Current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
    • F42B10/661—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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2233—Multimissile systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2253—Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2273—Homing guidance systems characterised by the type of waves
    • F41G7/2293—Homing guidance systems characterised by the type of waves using electromagnetic waves other than radio waves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/01—Arrangements thereon for guidance or control

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Electromagnetism (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Gyroscopes (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Preparation Of Compounds By Using Micro-Organisms (AREA)
  • Lasers (AREA)

Abstract

Es wird ein flügelstabilisierter Submunitionskörper (10) mit einer Zielerfassungsvorrichtung vorgeschlagen, der sich durch Verwendung eines starren Sensors (14) und eines dreiachsigen Laserkreisels (16) gegenüber bekannten Submunitionskörpern durch eine hohe Abschußfestigkeit und Zuverlässigkeit bei einfa­ chem Aufbau auszeichnet.
Zur Steuerung in einem Zielgebiet dienen Mikroreaktionstriebwer­ ke (18), die im Submunitionskörper (10) vor dessen Schwerpunkt angeordnet sind.
EP19890120959 1989-03-01 1989-11-11 Flügelstabilisierter Submunitionskörper Withdrawn EP0384965A3 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3906372 1989-03-01
DE3906372A DE3906372A1 (de) 1989-03-01 1989-03-01 Fluegelstabilisierter submunitionskoerper

Publications (2)

Publication Number Publication Date
EP0384965A2 EP0384965A2 (de) 1990-09-05
EP0384965A3 true EP0384965A3 (de) 1992-08-12

Family

ID=6375175

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19890120959 Withdrawn EP0384965A3 (de) 1989-03-01 1989-11-11 Flügelstabilisierter Submunitionskörper

Country Status (4)

Country Link
US (1) US5037040A (de)
EP (1) EP0384965A3 (de)
CA (1) CA2011046A1 (de)
DE (1) DE3906372A1 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11433999B2 (en) 2019-04-22 2022-09-06 Dalian University Of Technology Vehicle capable of taking off and landing vertically and operating in water, land, air and submarine environments

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5261629A (en) * 1989-04-08 1993-11-16 Rheinmetall Gmbh Fin stabilized projectile
DE29512894U1 (de) * 1995-08-10 1995-10-26 Mafo Systemtechnik Dr.-Ing. A. Zacharias GmbH & Co. KG, 83317 Teisendorf Waffe
US6502785B1 (en) * 1999-11-17 2003-01-07 Lockheed Martin Corporation Three axis flap control system
US20070089628A1 (en) * 2005-10-20 2007-04-26 Elder Steven M Firearm ammunition having improved flight and impact characteristics
RU2301957C1 (ru) * 2006-01-10 2007-06-27 Федеральное государственное унитарное предприятие "Государственный научно-исследовательский институт машиностроения" Осколочно-фугасная боевая часть
RU2301958C1 (ru) * 2006-01-10 2007-06-27 Федеральное государственное унитарное предприятие "Государственный научно-исследовательский институт машиностроения" Осколочно-фугасная боевая часть направленно-кругового действия
SE534614C2 (sv) * 2010-02-25 2011-10-25 Bae Systems Bofors Ab Granat anordnad med utfällbara vingar och styranordning
US9464876B2 (en) * 2014-05-30 2016-10-11 General Dynamics Ordnance and Tacital Systems, Inc. Trajectory modification of a spinning projectile by controlling the roll orientation of a decoupled portion of the projectile that has actuated aerodynamic surfaces

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3282540A (en) * 1964-05-05 1966-11-01 Henry S Lipinski Gun launched terminal guided projectile
EP0028966A1 (de) * 1979-11-09 1981-05-20 Thomson-Brandt Armements Verfahren zur Endphasenlenkung und -führung von Flugkörpern
EP0081421A1 (de) * 1981-12-09 1983-06-15 Thomson-Brandt Armements Verfahren zur Endphasenlenkung und dieses Verfahren verwendender Lenkflugkörper
DE3337873A1 (de) * 1982-10-18 1984-04-19 Raytheon Co., 02173 Lexington, Mass. Geschoss fuer granatwerfersysteme
US4598884A (en) * 1984-11-28 1986-07-08 General Dynamics Pomona Division Infrared target sensor and system

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3304434A (en) * 1965-06-01 1967-02-14 Bunker Ramo Position control system employing pulse producing means indicative of magnitude and direction of movement
US4533094A (en) * 1982-10-18 1985-08-06 Raytheon Company Mortar system with improved round

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3282540A (en) * 1964-05-05 1966-11-01 Henry S Lipinski Gun launched terminal guided projectile
EP0028966A1 (de) * 1979-11-09 1981-05-20 Thomson-Brandt Armements Verfahren zur Endphasenlenkung und -führung von Flugkörpern
EP0081421A1 (de) * 1981-12-09 1983-06-15 Thomson-Brandt Armements Verfahren zur Endphasenlenkung und dieses Verfahren verwendender Lenkflugkörper
DE3337873A1 (de) * 1982-10-18 1984-04-19 Raytheon Co., 02173 Lexington, Mass. Geschoss fuer granatwerfersysteme
US4598884A (en) * 1984-11-28 1986-07-08 General Dynamics Pomona Division Infrared target sensor and system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11433999B2 (en) 2019-04-22 2022-09-06 Dalian University Of Technology Vehicle capable of taking off and landing vertically and operating in water, land, air and submarine environments

Also Published As

Publication number Publication date
DE3906372C2 (de) 1991-06-27
EP0384965A2 (de) 1990-09-05
CA2011046A1 (en) 1990-09-01
DE3906372A1 (de) 1990-09-13
US5037040A (en) 1991-08-06

Similar Documents

Publication Publication Date Title
EP0384965A3 (de) Flügelstabilisierter Submunitionskörper
DE69104689D1 (de) Vorrichtung zur integrierten Steuerung der Längseigungs- und Schubachsen eines Luftfahrzeuges.
FR2458046A1 (fr) Fusee-detonateur de proximite pour missiles anti-chars
DE69104657D1 (de) Vorrichtung zur integrierten Steuerung der Längsneigungs- und Schubachsen eines Luftfahrzeuges.
EP1179296A3 (de) Vorrichtung zur Simulation einer lebenden Taube
DE3575578D1 (de) Verfahren zur pulvermetallurgischen herstellung von legierungen auf titanbasis mit kleiner korngroesse.
EP0296309A3 (de) Unterkalibriges flügelstabilisiertes Geschoss
Larina Protein composition in human plasma after long-term orbital missions and in rodent plasma after spaceflights on biosatellites" Cosmos-1887" and" Cosmos-2044"
DE3880281D1 (de) 5-nitro-4,6-bis-(3-nitro-1h-1,2,4-triazol-1-yl)pyrimidin, verfahren zu seiner herstellung und dieses enthaltender sprengstoff.
RU96113157A (ru) Сверхзвуковая управляемая ракета
EP0389855A3 (de) Am Boden eines Submunitionen enthaltenden Trägerprojektils befestigtes Bremstuch
Svensson A simple method for accurate position determination of birds on open ground.
Zur Neither doves nor hawks: Marking the territory covered by the field of the psychology of peace and war: I.
ATE36123T1 (de) Vorrichtung zur abgabe wenigstens eines konzentrats fuer wenigstens eine zugabe zu einem loesungsmittel, auch mit betaetigungseinrichtung.
BOURA et al. AQM: Accelerometer for precision-guided weapons(LAQM: ACCELEROMETRE POUR MUNITIONS DE PRECISION)
Lkhagva Diurnal rhythm of body temperature during space flight
GELIN Pyrophoric alkylaluminum compounds in decoy flares
THOMSEN et al. Impact cratering calculations. Part 1: Early time results[Interim Final Report]
TIERNO Simulating the movement of tactical missiles(Simulacion del movimiento de misiles tacticos)
Jeziorski High and dry
POPE Further analysis of yawsonde data from some liquid payload projectiles[Final Report]
RUSSELL et al. Incoflex two axes accelerometer program[Final Report, 22 Jun. 1976- 26 Jul. 1977]
Higashi Ukichiro Nakaya—1900–1962
IT1118364B (it) Cava bulbi e simili,specialmente adatto per la raccolta dei porri,costituito da un vomere la cui lamaha un andamento di attacco quasi orizzontale collegato ad un versoio concavo di circa 90'
DAVIS Illumination requirements for target recognition and reacquisition as a function of field of view(visual tasks)

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): DE FR GB IT SE

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): DE FR GB IT SE

RAP3 Party data changed (applicant data changed or rights of an application transferred)

Owner name: RHEINMETALL GMBH

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 19930213