EP0223919B1 - Procédé et application de sous-munition à guidage terminal pour la lutte contre abris blindés - Google Patents

Procédé et application de sous-munition à guidage terminal pour la lutte contre abris blindés Download PDF

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Publication number
EP0223919B1
EP0223919B1 EP86110414A EP86110414A EP0223919B1 EP 0223919 B1 EP0223919 B1 EP 0223919B1 EP 86110414 A EP86110414 A EP 86110414A EP 86110414 A EP86110414 A EP 86110414A EP 0223919 B1 EP0223919 B1 EP 0223919B1
Authority
EP
European Patent Office
Prior art keywords
submunition
sensor
apron
shelter
door
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.)
Expired - Lifetime
Application number
EP86110414A
Other languages
German (de)
English (en)
Other versions
EP0223919A1 (fr
Inventor
Peter Dr. Sundermeyer
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 Verwaltungs Stiftung
Original Assignee
Diehl GmbH and Co
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 GmbH and Co filed Critical Diehl GmbH and Co
Publication of EP0223919A1 publication Critical patent/EP0223919A1/fr
Application granted granted Critical
Publication of EP0223919B1 publication Critical patent/EP0223919B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • F41G7/2226—Homing guidance systems comparing the observed data with stored target data, e.g. target configuration data
    • 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
    • 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
    • F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
    • F42B12/10—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge
    • F42B12/14—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge the symmetry axis of the hollow charge forming an angle with the longitudinal axis of the projectile

Definitions

  • the invention relates to a method according to the preamble of claim 1 and its preferred implementation by using submunition according to claim 11.
  • tandem charge is already ignited within the ground, at a distance from the concrete jacket, this piercing is no longer to be expected; because the effect of the tandem charge essentially only unfolds itself when the concrete body penetrates, but dissipates in the upstream soil.
  • the object of the invention is to create an anti-shelter weapon which - if possible even with less ammunition expenditure - promises greater effectiveness.
  • Such a forecourt is relatively easy to spot with a target search detector, as it, as a large asphalt or concrete surface, differs significantly from the clutter picked up on board the ammunition, which consists of the bushes, the lawn and the sand in the vicinity of the square in front of the shelter gate comes from. Maneuver commands for the final phase flight correction of the submunition can thus be derived from the sensor information in order to steer the latter into the center of a shelter forecourt during a steep final approach.
  • the probability of hits - with regard to the wall space between a shelter gate and the connection path to the runways - is further increased if the sensor for the final phase maneuvers is designed in addition to pattern recognition, for example to widen the connection path to the turning forecourt and / or the typically roughly curved and to process radiation-like splinter protection hill structure, which surrounds such turning space, as a target criterion, without having to drive the signal processing expenditure for the detection of construction details, which are typical for the protrusion of a bunker roof over the shelter gate, but which, on the other hand, can easily be removed by ent speaking design of the earth walls lying directly above can be camouflaged.
  • a gate detection can be provided, which is based on using the control sensor oriented obliquely in advance or using an approximately horizontally oriented additional sensor to acquire the limited flat area of the shelter gate between adjoining splinter protection earth walls, in order to acquire approximately to ignite horizontally oriented projectile-forming charge when it rotates with the rotating ammunition in the direction of the detected gate.
  • a submunition is therefore particularly suitable in the context of the present invention, a missile which can be corrected for the end phase and which, in the case of a steep descent in the target area, preferably spirally scans it, preferably with its own movement with at least one rigidly installed sensor, in order to detect the target (here primarily the shelter forecourt) by means of temporary adjustment of control rudders to make a path correction, as described for an implementation example in EP-OS 81 421. Because the effect in the target no longer depends on the submunition accidentally hitting a shelter at a suitable point, but because the space in front of the most vulnerable shelter area, namely in front of its gate, is now targeted, is for equal effectiveness Ammunition requires much less effort, e.g.
  • Carriers in the form of projectiles, missiles or airplanes are suitable for this shipment; however, the shipment is preferably carried out using a distance weapon carrier that can be released from the aircraft, as described, for example, in WEHRTECHNIK 5/84 (page 116, top left).
  • the detection of the target in the form of the widened, relatively flat space (and possibly the flat gate of limited area) in the significantly different clutter-producing environment is carried out, for example, according to the criteria explained in DE-OS 34 34 326.
  • the warhead of the submunition has an essentially cylindrical structure, the cylinder axis of which is pivoted by the function-typical angle of incidence of the submunition into the target area relative to the longitudinal axis of the submunition, so that it is aligned as perpendicularly as possible at the point of impact.
  • projectile-forming coverings arranged along the cylinder wall lead to projectiles which are fired essentially horizontally; At least one of them strikes the shelter’s armored gate essentially vertically and pierces it with glowing splinters in order to put the aircraft parked behind it out of action.
  • more than three, typically about six projectile-forming assignments on the warhead are arranged peripherally offset from one another.
  • the warhead can also be equipped with a pre-existing assignment, in order to additionally break open the shelter forecourt in the vicinity of the point of impact of the submunition, that is to say make it impassable.
  • a so-called multi-purpose warhead as described, for example, in its own older patent DE-C-35 25 147 for a cylinder jacket assignment that has been specifically optimized with regard to another application, as is also known from DE-B 1578089 is known, is described in more detail.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Claims (12)

1. Procédé pour attaquer des abris de surface blindés, notamment des abris pour avions, caractérisé en ce qu'on détecte une avant-place située devant la porte de l'abri et qu'on oriente vers elle une tête de combat en approche terminale très inclinée, à la suite de quoi la tête de combat tire vers la porte, dans une direction sensiblement horizontale, une garniture formant des projectiles.
2. Procédé selon la revendication 1, caractérisé en ce qu'on prévoit plusieurs garnitures radiales, décalées l'une par rapport à l'autre sur la périphérie, sur la sous-munition prévue pour le vol en piqué.
3. Procédé selon la revendication 2, caractérisé en ce que la tête de combat comporte en outre une composante active préorientée.
4. Procédé selon la revendication 1, 2 ou 3, caractérisé en ce qu'on oriente vers l'avant-place une sous-munition pouvant être manoeuvrée en phase terminale.
5. Procédé selon la revendication 4, caractérisé en ce que les manoeuvres de phase terminale sont commandées par un détecteur qui évalue la différence significative entre les échos parasites de l'avant-place d'une part, et ceux du terrain, notamment le terrain couvert de végétation qui l'entoure, d'autre part.
6. Procédé selon la revendication 4 ou 5, caractérisé en ce que les manoeuvres de phase terminale sont commandées par un détecteur qui évalue le profil des reliefs typique dans l'entourage de l'avant-place.
7. Procédé selon l'une des revendications 4 à 6, caractérisé en ce que les manoeuvres de phase terminale sont commandées par un détecteur qui explore en spirale la zone de la cible pour acquérir le centre de l'avant-place.
8. Procédé selon la revendication 7, caractérisé en ce que le détecteur est incorporé solidaire, dans une sous-munition qui descend dans la zone de la cible en faisant des cercles.
9. Procédé selon l'une des revendications 5 à 8, caractérisé en ce qu'on prévoit un détecteur qui évalue la différence significative entre les échos parasites de la porte, d'une part, et ceux du terrain qui l'avoisine, notamment du terrain couvert de végétation, d'autre part et met à feu une charge formant des projectiles, lors du basculement dans la ligne de visée orientée vers la porte.
10. Procédé selon l'une des revendications 4 à 9, caractérisé en ce que la sous-munition est aménée au dessus de la zone de la cible au moyen d'un porteur manoeuvrant par lui-même.
11. Utilisation d'une sous-munition descendant sous un angle très fort, à correction de phase terminale et comportant au moins une garniture formant des projectiles, orientée sensiblement transversalement à un axe longitudinal et un détecteur de manoeuvre répondant au centre de la signature typique d'échos parasites de l'avant-place située devant des abris de surface blindés, pour mettre en oeuvre le procédé selon l'une des revendications précédentes.
12. Utilisation de la sous-munition selon la revendication 11, comportant un détecteur détectant la porte de l'abri pour mettre à feu avec correction d'orientation, une charge située dans la sous-munition, orientée sensiblement horizontalement et projetant des projectiles.
EP86110414A 1985-08-01 1986-07-28 Procédé et application de sous-munition à guidage terminal pour la lutte contre abris blindés Expired - Lifetime EP0223919B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3527522 1985-08-01
DE19853527522 DE3527522A1 (de) 1985-08-01 1985-08-01 Verfahren und verwendung von endphasenkorrigierter submunition zum bekaempfen von gepanzerten unterstaenden

Publications (2)

Publication Number Publication Date
EP0223919A1 EP0223919A1 (fr) 1987-06-03
EP0223919B1 true EP0223919B1 (fr) 1990-06-13

Family

ID=6277326

Family Applications (1)

Application Number Title Priority Date Filing Date
EP86110414A Expired - Lifetime EP0223919B1 (fr) 1985-08-01 1986-07-28 Procédé et application de sous-munition à guidage terminal pour la lutte contre abris blindés

Country Status (3)

Country Link
US (1) US4831935A (fr)
EP (1) EP0223919B1 (fr)
DE (2) DE3527522A1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2636419B1 (fr) * 1988-09-09 1993-10-01 Thomson Brandt Armements Projectile de neutralisation de zone, notamment d'aerodrome
DE3919573A1 (de) * 1989-06-15 1990-12-20 Diehl Gmbh & Co Verfahren und einrichtung zur akquisition eines zielpunktes
DE4007677C1 (de) * 1990-03-10 1998-05-14 Diehl Gmbh & Co Vorrichtung zum Bekämpfen von insbes. für Fluggeräte vorgesehenen gepanzerten Unterständen
DE4123485A1 (de) * 1991-07-16 1993-01-21 Rheinmetall Gmbh Vorrichtung zur bekaempfung von flugzeugen in sheltern
EP0800054B1 (fr) * 1996-04-05 2001-09-19 Luchaire Défense S.A. Projectile dont la charge explosive est déclenchée au moyen d'un désignateur de cible
JP6492101B2 (ja) 2014-03-04 2019-03-27 シンジェンタ パーティシペーションズ アーゲー 殺微生物性二環式複素環式誘導体

Family Cites Families (20)

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Publication number Priority date Publication date Assignee Title
GB1458809A (en) * 1957-10-24 1976-12-15 Mini Defence Missile warheads
US4063512A (en) * 1966-10-05 1977-12-20 The United States Of America As Represented By The Secretary Of The Air Force Armor penetrating projectile
DE1578089B1 (de) * 1967-10-14 1975-07-03 Messerschmitt Boelkow Blohm Gefechtskopf fuer einen raketengetriebenen Flugkoerper oder ein Geschoss zur Bekaempfung von gepanzerten Zielen
US4175491A (en) * 1966-10-08 1979-11-27 Messerschmitt-Bolkow-Blohm Gesellschaft Mit Beschrankter Haftung Warhead and anti-tank missile construction
US3948175A (en) * 1970-02-03 1976-04-06 Dynamit Nobel Aktiengesellschaft Warhead
US3978797A (en) * 1971-04-28 1976-09-07 The United States Of America As Represented By The Secretary Of The Navy Radiometric target detection device
DE2156974A1 (de) * 1971-11-17 1979-09-06 Messerschmitt Boelkow Blohm Behaelter zur aufnahme von streuwaffen, die am einsatzort aus dem von einem flugzeug getragenen behaelter ausgestossen werden
US4050381A (en) * 1972-04-12 1977-09-27 The United States Of America As Represented By The Secretary Of The Army Low density indirect fire munition system (U)
US4522356A (en) * 1973-11-12 1985-06-11 General Dynamics, Pomona Division Multiple target seeking clustered munition and system
DE2629280C1 (de) * 1976-06-30 1985-07-25 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Gefechtskopf zum Bekaempfen von Zielobjekten,insbesondere Flugzeugen,die in Schutzraeumen untergebracht sind
US4492166A (en) * 1977-04-28 1985-01-08 Martin Marietta Corporation Submunition having terminal trajectory correction
DE2838347A1 (de) * 1978-09-02 1980-03-20 Rheinmetall Gmbh Gefechtskopf mit in einem abschussrohr angeordneten tochtergeschossen
FR2552870B1 (fr) * 1980-10-24 1987-02-13 France Etat Armement Perfectionnement aux tetes militaires a charges formees montees en tandem
US4565341A (en) * 1981-09-24 1986-01-21 Zacharin Alexey T Inflatable decelerator
FR2517818A1 (fr) * 1981-12-09 1983-06-10 Thomson Brandt Methode de guidage terminal et missile guide operant selon cette methode
DE3306659A1 (de) * 1983-02-25 1984-08-30 Rheinmetall GmbH, 4000 Düsseldorf Wirkkoerpereinheit
DE3322927A1 (de) * 1983-06-25 1985-01-03 Rheinmetall GmbH, 4000 Düsseldorf Von einem lastengeschoss oder flugkoerper abwerfbarer geschosskopf
US4554871A (en) * 1983-11-21 1985-11-26 Allied Corporation Dispensed guided submunition
DE3434326C2 (de) * 1984-09-19 1995-03-09 Deutsche Aerospace Verfahren zur Ableitung einer clutterabhängigen Zielerkennungsschwelle in einer Radaranlage
DE3522154A1 (de) * 1985-06-21 1987-01-02 Diehl Gmbh & Co Suchzuender-submunition

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
"WEHRTECHNIK" 84/5, Seiten 115-117 *

Also Published As

Publication number Publication date
US4831935A (en) 1989-05-23
EP0223919A1 (fr) 1987-06-03
DE3527522C2 (fr) 1988-11-24
DE3671957D1 (de) 1990-07-19
DE3527522A1 (de) 1987-02-12

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