EP1674818B1 - Missile - Google Patents

Missile Download PDF

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Publication number
EP1674818B1
EP1674818B1 EP20050027434 EP05027434A EP1674818B1 EP 1674818 B1 EP1674818 B1 EP 1674818B1 EP 20050027434 EP20050027434 EP 20050027434 EP 05027434 A EP05027434 A EP 05027434A EP 1674818 B1 EP1674818 B1 EP 1674818B1
Authority
EP
European Patent Office
Prior art keywords
missile
target
power microwave
hlm
microwave pulses
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.)
Revoked
Application number
EP20050027434
Other languages
German (de)
English (en)
Other versions
EP1674818A1 (fr
Inventor
Peter Gleich
Erich Waxweiler
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.)
LFK Lenkflugkoerpersysteme GmbH
Original Assignee
LFK Lenkflugkoerpersysteme 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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=35840438&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=EP1674818(B1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by LFK Lenkflugkoerpersysteme GmbH filed Critical LFK Lenkflugkoerpersysteme GmbH
Publication of EP1674818A1 publication Critical patent/EP1674818A1/fr
Application granted granted Critical
Publication of EP1674818B1 publication Critical patent/EP1674818B1/fr
Revoked legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H13/00—Means of attack or defence not otherwise provided for
    • F41H13/0043—Directed energy weapons, i.e. devices that direct a beam of high energy content toward a target for incapacitating or destroying the target
    • F41H13/0068—Directed energy weapons, i.e. devices that direct a beam of high energy content toward a target for incapacitating or destroying the target the high-energy beam being of microwave type, e.g. for causing a heating effect in the target
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information

Definitions

  • the invention relates to a missile according to the preamble of claim, such a device is made DE 199 59 358 known.
  • missiles There are numerous embodiments of missiles for a variety of applications known. In modern conflict scenarios increasingly attack missions of so-called. "Cheap drones" are described, which are equipped with chemical or biological weapons, z. For example, in future out-of-area missions, they could pose an immense potential threat to troops.
  • a generic missile with a fuselage, a power supply device, a high-power microwave generator for generating HLM pulses and a directional antenna for spatially directed delivery of the HLM pulses is in the US 5,192,827 disclosed.
  • HLM high-power microwave
  • the missile can effectively serially combat multiple attack drones by disrupting or destroying their electronic components and forcing them to crash or missions abort.
  • the HLM missile After being instructed by external sensor systems (eg ground / airborne radars), the HLM missile navigates autonomously to a target expectation area, which by higher-level sensor / fire control systems from the target position and Target speed was calculated. During its flight there, the target heading of the missile is updated externally at regular intervals.
  • external sensor systems eg ground / airborne radars
  • the on-board sensor takes over the search for the target and guides the missile closer to the target by means of a prescribed steering law.
  • a defined approach geometry must be maintained, which allows a directed to the target radiation of the HLM pulses by means of rigidly installed FK antennas.
  • the control of the missile is carried out by aerodynamic bow or stern rudder, the control concept corresponds to the classic "bank to turn" principle of single wing aircraft.
  • the two variants are in the FIGS. 1a and 1b respectively. 2a and 2b shown.
  • the autopilot converts the steering commands in the marching phase and in the final steering phase into the corresponding control commands in a known manner.
  • Superordinate ground or airborne sensors detect approaching drones, their position, heading and speed are measured and forwarded to an appropriate launch facility for HLM missiles.
  • the selected HLM missile is programmed with a first estimate of the target expectation space (target and missile position at the meeting).
  • the missile is launched by solids discharge booster or by catapult, the jet engine runs high, the starting booster is dropped and the missile heads for the roughly calculated target expectation space.
  • the use of a start booster is not necessary, if in principle should be started with the help of a catapult.
  • the target expectation space is permanently updated by the external target measurement the missile will be informed by data link the resulting course corrections.
  • the on-board end-phase sensor takes over the FK steering, as described above.
  • the FK is trained on the next target u.s.w ..
  • the FK autonomously enters the march back to the predetermined or data link commanded landing.
  • the missile can be launched after a general function check, the installation of a new booster and after refueling to another mission.
  • the missile can be used in addition to the focus task of drone hunting for other missions in which the destruction / destruction of relatively little shielded electronic components is intended.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Claims (1)

  1. Engin volant comprenant un fuselage, un dispositif d'alimentation en énergie, un générateur d'hyperfréquences de grande puissance pour générer des impulsions HGP et une antenne directionnelle pour délivrer les impulsions HGP de manière directionnelle dans l'espace, caractérisé en ce qu'il présente un groupe propulseur, un réservoir de carburant ainsi que des surfaces de sustentation et de contrôle agissant aérodynamiquement,
    une électronique de navigation, de direction et de régulation,
    un dispositif de communication pour l'échange de données avec une centrale de commande,
    un détecteur de phase finale pour le guidage dans la zone de proximité de la cible
    et que pour pouvoir être réutilisé, il présente un blindage pour les équipements électroniques contre les impulsions HGP générées et
    un système de récupération à parachute/parapente.
EP20050027434 2004-12-23 2005-12-15 Missile Revoked EP1674818B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE200410061979 DE102004061979B4 (de) 2004-12-23 2004-12-23 Flugkörper

Publications (2)

Publication Number Publication Date
EP1674818A1 EP1674818A1 (fr) 2006-06-28
EP1674818B1 true EP1674818B1 (fr) 2010-07-21

Family

ID=35840438

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20050027434 Revoked EP1674818B1 (fr) 2004-12-23 2005-12-15 Missile

Country Status (2)

Country Link
EP (1) EP1674818B1 (fr)
DE (2) DE102004061979B4 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE530922C2 (sv) * 2007-05-29 2008-10-21 Totalfoersvarets Forskningsinstitut Tandemstridsdel för användning mot mål med elektriska system
SE530927C2 (sv) * 2007-05-29 2008-10-21 Totalfoersvarets Forskningsinstitut Stridsdel för användning mot mål med elektriska system
DE102007054382A1 (de) * 2007-11-14 2009-05-20 Diehl Bgt Defence Gmbh & Co. Kg De-Letalisierbare Munition
DE102013006812B4 (de) * 2013-04-19 2015-01-15 Mbda Deutschland Gmbh Lenkflugkörper sowie Wirksystem, umfassend den Lenkflugkörper

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1591681A1 (de) * 1967-06-09 1971-01-14 Telefunken Patent Luftfahrzeug mit einer Bordantenne
US5192827A (en) * 1991-12-19 1993-03-09 The United States Of America As Represented By The Secretary Of The Army Microwave projectile
DE10044867A1 (de) * 2000-09-12 2002-03-21 Rheinmetall W & M Gmbh Explosivstoffgetriebene RF-Strahlenquelle

Also Published As

Publication number Publication date
DE502005009943D1 (de) 2010-09-02
EP1674818A1 (fr) 2006-06-28
DE102004061979A1 (de) 2006-07-06
DE102004061979B4 (de) 2009-10-29

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