EP1783451B1 - Spin-stabilised artillery projectile - Google Patents

Spin-stabilised artillery projectile Download PDF

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Publication number
EP1783451B1
EP1783451B1 EP06022695A EP06022695A EP1783451B1 EP 1783451 B1 EP1783451 B1 EP 1783451B1 EP 06022695 A EP06022695 A EP 06022695A EP 06022695 A EP06022695 A EP 06022695A EP 1783451 B1 EP1783451 B1 EP 1783451B1
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EP
European Patent Office
Prior art keywords
projectile
artillery projectile
artillery
elements
target area
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EP06022695A
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German (de)
French (fr)
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EP1783451A3 (en
EP1783451A2 (en
Inventor
Karl Kautzsch
Albrecht Reindler
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Junghans Microtec GmbH
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Junghans Microtec GmbH
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Publication of EP1783451A3 publication Critical patent/EP1783451A3/en
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    • 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
    • F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
    • F42B10/50—Brake flaps, e.g. inflatable
    • 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

Definitions

  • the invention relates to a spin stabilized artillery projectile according to the preamble of claim 1.
  • Such a spin stabilized artillery projectile is from the DE 101 43 312 C1 and from DE 102 42 588 B4 known.
  • This artillery projectile has in its ogive a radially acting braking device, which serves to reduce the longitudinal shelf of the artillery projectile in a target area. This makes a 1D correction possible.
  • the storage area of an artillery projectile in a target area is elliptical, so it has a longitudinal axis and a transverse axis orthogonal thereto.
  • the longitudinal axis, i. the longitudinal tray is larger than the transverse axis, i. the cross shelf.
  • the braking device of the known spin-stabilized artillery projectile serves to reduce the large lengthwise deposit of the artillery projectile in the target area compared to the crossbeam and thus to improve the accuracy of the target accordingly.
  • the invention has for its object to provide a spin stabilized artillery projectile of the type mentioned, in which reduced by simple means and the cross-placement of the artillery projectile in the target area and thus the accuracy is improved accordingly.
  • the momentum elements can be provided in the ogive of the artillery projectile.
  • the pulse elements may be formed by the pyrotechnic force elements, which are associated with a front annular region of a hood covering the braking device, and by means of which the hood of the ogive of the artillery projectile can be abspengbar.
  • Such impulse elements in the form of pyrotechnic force elements are quoted in the opening paragraph DE 101 43 312 C1 described.
  • the pulse elements are provided on a ring element which is arranged between the projectile fuse and the projectile housing.
  • the impulse elements in the tail section i. in Base Bleed, the artillery projectile.
  • This device can be provided in the artillery projectile, so that there is a self-sufficient device and a self-sufficient artillery projectile. Another possibility is that this device is controlled by satellite.
  • a satellite-based control of a web-corrected spin-stabilized artillery projectile of the type mentioned, ie for the reduction of the longitudinal storage of the artillery projectile in a target area, is in the EP 1 103 779 B1 described, their disclosure content, which concerns the targeted activation of the impulse elements provided at the periphery of the artillery projectile in order to reduce the cross-placement of the artillery projectile in a target area, forms part of the present invention.
  • the web-correctable spin-stabilized artillery projectile according to the invention has the advantage that, with structurally simple means, in addition to the reduction of the longitudinal deposit, a reduction of the transverse placement of the artillery projectile in a target area is realized.
  • the reduction of the cross-shelf, i. the controlled page correction of the artillery projectile, carried out before the activation of the braking device for reducing the longitudinal storage of the artillery projectile in the target area because the page correction is faster in time as the braking device for reducing the longitudinal shelf is effective.
  • FIG. 1 shows longitudinally sectioned the front portion of a formation of the spin-stabilized artillery projectile 10 with a provided in its ogive 12 projectile detonator 14 and a provided in the ogive 12 braking device 16 which is centrifugally force adjustable by pyrotechnic force elements 18, which are associated with a front ring portion 20 of a hood 22.
  • the pyrotechnic force elements 18 form impulse elements 24 of the artillery projectile 10, which are arranged distributed uniformly on the circumference of the artillery projectile.
  • the braking device 16 serves to reduce the longitudinal storage of the artillery projectile 10 in a target area (see the Figures 3 and 4 ).
  • FIG. 4 is the target area 26 elliptical, ie with an elliptical edge 28, illustrated.
  • the limited by the elliptical edge 28 shelf 30 has a longitudinal axis A 0 and a transverse axis B 0 .
  • the braking device 16 results in a reduction of the longitudinal shelf, ie the longitudinal axis A 0 , to an amount A r .
  • a reduction of the transverse axis B 0 is not effected by the braking device 16 of the artillery projectile 10, ie by the braking device 16, the storage surface 30 is reduced to a storage surface 32 which is bounded by the edge line 34.
  • pulse elements 24 is obtained by appropriate activation of the corresponding pulse elements 24 in an artillery projectile 10 with braking device 16, a reduction of the cross-stock of the artillery projectile 10, ie a further reduction of the storage surface 32 to a storage area 36 through the Edge line 38 is limited.
  • the support surface 36 is determined in the x-direction by the longitudinal dimension A r and in the y-direction by the transverse dimension B r , wherein it is preferred if A r and B r are the same size, so that a circular support surface 36 results.
  • FIG. 2 clarifies a training of the artillery projectile 10 in one of FIG. 1 similar cutaway longitudinal sectional view, wherein the pulse elements 24 are provided on a ring member 40 in the circumferential direction uniformly distributed, the is arranged between the projectile fuze 14 and the projectile housing 42.
  • the pyrotechnic force elements 18 are used in this embodiment of the artillery projectile 10 only for blowing off the brake device 16 covering the hood 22nd
  • the impulse elements in the rear part (base bleed) of the artillery projectile 10 may be distributed evenly in the circumferential direction.
  • FIG. 3 is designated reference numeral 50 a Feuerleitrechner.
  • the fire control computer 50 determines the azimuth orientation, the elevation indicated by the double arrow 52, and the propellant power, ie, the theoretical exit velocity 54 for the ballistic trajectory 56 of the artillery projectile 10 into the target area, depending on the pre-enlightened direction and distance 44 from a gun 48 to a target 46 26th

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  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Braking Arrangements (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Steroid Compounds (AREA)

Abstract

A spin-stabilized artillery projectile (10) has a projectile detonator (14) provided in an ogive (12) of the projectile; a radially deployed brake device (16) provided in the ogive for reduction of a longitudinal deviation (A o, A r) of the projectile in a target area; and a number of impulse elements (24) distributed around a circumference of the projectile to reduce a lateral deviation (B o, B r) of the projectile in the target area. The impulse elements are formed by pyrotechnic force elements (18) associated with a front ring area (20) of a shroud (22) covering the brake device.

Description

Die Erfindung betrifft ein drallstabilisiertes Artillerieprojektil gemäß dem Oberbegriff des Anspruches 1.The invention relates to a spin stabilized artillery projectile according to the preamble of claim 1.

Ein derartiges drallstabilisiertes Artillerieprojektil ist aus der DE 101 43 312 C1 und aus DE 102 42 588 B4 bekannt. Dieses Artillerieprojektil weist in seiner Ogive eine radial anstellende Bremseinrichtung auf, die zur Reduktion der Längsablage des Artillerieprojektiles in einem Zielgebiet dient. Damit ist eine 1 D-Korrektur möglich.Such a spin stabilized artillery projectile is from the DE 101 43 312 C1 and from DE 102 42 588 B4 known. This artillery projectile has in its ogive a radially acting braking device, which serves to reduce the longitudinal shelf of the artillery projectile in a target area. This makes a 1D correction possible.

Die Ablagefläche eines Artillerieprojektiles in einem Zielgebiet ist ellipsenförmig, sie weist also eine Längsachse und eine dazu orthogonale Querachse auf. Die Längsachse, d.h. die Längsablage, ist größer als die Querachse, d.h. die Querablage. Die Bremseinrichtung des bekannten drallstabilisierten Artillerieprojektiles dient dazu, die im Vergleich zur Querablage große Längsablage des Artillerieprojektiles im Zielgebiet zu reduzieren und somit die Zielgenauigkeit entsprechend zu verbessern.The storage area of an artillery projectile in a target area is elliptical, so it has a longitudinal axis and a transverse axis orthogonal thereto. The longitudinal axis, i. the longitudinal tray is larger than the transverse axis, i. the cross shelf. The braking device of the known spin-stabilized artillery projectile serves to reduce the large lengthwise deposit of the artillery projectile in the target area compared to the crossbeam and thus to improve the accuracy of the target accordingly.

Der Erfindung liegt die Aufgabe zugrunde, ein drallstabilisiertes Artillerieprojektil der eingangs genannten Art zu schaffen, bei dem mit einfachen Mitteln auch die Querablage des Artillerieprojektiles im Zielgebiet reduziert und somit die Zielgenauigkeit entsprechend verbessert ist.The invention has for its object to provide a spin stabilized artillery projectile of the type mentioned, in which reduced by simple means and the cross-placement of the artillery projectile in the target area and thus the accuracy is improved accordingly.

Diese Aufgabe wird erfindungsgemäß durch die Merkmale des Anspruches 1 gelöst. Bevorzugte Aus- bzw. Weiterbildungen des erfindungsgemäßen bahnkorrigierenden drallstabilisierten Artillerieprojektiles sind in den Unteransprüchen gekennzeichnet.This object is achieved by the features of claim 1. Preferred embodiments or further developments of the sheet-correcting spin-stabilized artillery projectile according to the invention are characterized in the subclaims.

Dadurch, dass bei dem erfindungsgemäßen drallstabilisierten Artillerieprojektil am Umfang verteilt eine Anzahl Impulselemente vorgesehen sind, ist es möglich, durch passende Aktivierung mindestens eines entsprechenden Impulselementes eine Reduktion der Querablage des Artillerieprojektiles im Zielgebiet zu bewirken. Mit dem erfindungsgemäßen Artillerieprojektil wird zusätzlich zur Reduktion der Längsablage auch eine Reduktion der Querablage des Artillerieprojektiles im Zielgebiet und somit auf relativ einfache Weise eine wesentliche Verbesserung der Zielgenauigkeit realisiert. Vorteilhaft ist es hierbei, wenn die Impulselemente am Umfang des Artillerieprojektiles gleichmäßig verteilt angeordnet sind, weil dann die Ansteuerung des jeweils passenden Impulselementes vergleichsweise einfach möglich ist.Characterized in that in the spin-stabilized artillery projectile invention distributed around the circumference a number of impulse elements are provided, it is possible by appropriate activation of at least one corresponding impulse element to effect a reduction of the cross-placement of the artillery projectile in the target area. With the artillery projectile according to the invention, in addition to the reduction of the longitudinal storage, a reduction of the cross-placement of the artillery projectile in the target area and thus in a relatively simple manner, a substantial improvement in the accuracy of the target is realized. It is advantageous in this case if the pulse elements are arranged distributed uniformly on the circumference of the artillery projectile, because then the control of each matching pulse element is comparatively easily possible.

Bei dem erfindungsgemäßen drallstabilisierten Artillerieprojektil können die Impulselemente in der Ogive des Artillerieprojektiles vorgesehen sein. Bei einer derartigen Ausbildung können die Impulselemente von den pyrotechnischen Kraftelementen gebildet sein, die einem vorderen Ringbereich einer die Bremseinrichtung bedeckenden Haube zugeordnet sind, und mittels welchem die Haube von der Ogive des Artillerieprojektiles absprengbar ist. Derartige Impulselemente in Gestalt pyrotechnischer Kraftelemente sind in der eingangs zitierten DE 101 43 312 C1 beschrieben.In the spin-stabilized artillery projectile according to the invention, the momentum elements can be provided in the ogive of the artillery projectile. With such a design, the pulse elements may be formed by the pyrotechnic force elements, which are associated with a front annular region of a hood covering the braking device, and by means of which the hood of the ogive of the artillery projectile can be abspengbar. Such impulse elements in the form of pyrotechnic force elements are quoted in the opening paragraph DE 101 43 312 C1 described.

Bei dem Artillerieprojektil nach Anspruch 1 sind die Impulselemente an einem Ringelement vorgesehen, das zwischen dem Projektilzünder und dem Projektilgehäuse angeordnet ist. Hierdurch kann das Artillerieprojektil quasi unverändert mit einem bekannten Projektilzünder kombiniert werden .In the artillery projectile according to claim 1, the pulse elements are provided on a ring element which is arranged between the projectile fuse and the projectile housing. As a result, the artillery projectile can be virtually unchanged combined with a known projectile fuze.

Insbesondere bei Artillerieprojektilen großer Reichweite kann es bevorzugt sein, wenn die Impulselemente im Heckteil, d.h. im Base Bleed, des Artillerieprojektiles vorgesehen sind.Especially with long range artillery projectiles, it may be preferred if the impulse elements in the tail section, i. in Base Bleed, the artillery projectile.

Zur Bestimmung der jeweiligen zeitlichen Drehwinkelposition des Artillerieprojektiles und somit der an seinem Umfang verteilt vorgesehenen Impulselemente dient eine Einrichtung, die mit den Impulselementen, zu deren gezielter Aktivierung, zusammenwirkt. Diese Einrichtung kann im Artillerieprojektil vorgesehen sein, so dass sich eine autarke Einrichtung und ein autarkes Artillerieprojektil ergibt. Eine andere Möglichkeit besteht darin, dass diese Einrichtung satellitengestützt gesteuert wird. Eine satellitengestützte Steuerung eines bahnkorrigierbaren drallstabilisierten Artillerieprojektiles der eingangs genannten Art, d.h. zur Reduktion der Längsablage des Artillerieprojektiles in einem Zielgebiet, ist in der EP 1 103 779 B1 beschrieben, deren Offenbarungsgehalt, was die gezielte Aktivierung der am Umfang des Artillerieprojektiles vorgesehenen Impulselemente zur Reduktion der Querablage des Artillerieprojektiles in einem Zielgebiet anbelangt, Teil der vorliegenden Erfindung ist.To determine the respective angular position of rotation of the artillery projectile and thus distributed on its circumference provided impulse elements is a device that interacts with the pulse elements to their specific activation. This device can be provided in the artillery projectile, so that there is a self-sufficient device and a self-sufficient artillery projectile. Another possibility is that this device is controlled by satellite. A satellite-based control of a web-corrected spin-stabilized artillery projectile of the type mentioned, ie for the reduction of the longitudinal storage of the artillery projectile in a target area, is in the EP 1 103 779 B1 described, their disclosure content, which concerns the targeted activation of the impulse elements provided at the periphery of the artillery projectile in order to reduce the cross-placement of the artillery projectile in a target area, forms part of the present invention.

Das erfindungsgemäße bahnkorrigierbare drallstabilisierte Artillerieprojektil weist den Vorteil auf, dass mit konstruktiv einfachen Mitteln zusätzlich zur Reduktion der Längsablage eine Reduktion der Querablage des Artillerieprojektiles in einem Zielgebiet verwirklicht wird. Dabei wird die Reduktion der Querablage, d.h. die gesteuerte Seitenkorrektur des Artillerieprojektiles, zeitlich vor der Aktivierung der Bremseinrichtung zur Reduktion der Längsablage des Artillerieprojektiles im Zielgebiet durchgeführt, weil die Seitenkorrektur zeitlich schneller erfolgt als die Bremseinrichtung zur Reduktion der Längsablage wirksam wird.The web-correctable spin-stabilized artillery projectile according to the invention has the advantage that, with structurally simple means, in addition to the reduction of the longitudinal deposit, a reduction of the transverse placement of the artillery projectile in a target area is realized. Thereby, the reduction of the cross-shelf, i. the controlled page correction of the artillery projectile, carried out before the activation of the braking device for reducing the longitudinal storage of the artillery projectile in the target area, because the page correction is faster in time as the braking device for reducing the longitudinal shelf is effective.

Während bei dem bekannten drallstabilisierten Artillerieprojektil mit einer Reduktion der Längsablage also eine 1D-Korrektur erfolgt, ergibt sich beim erfindungsgemäßen Artillerieprojektil eine 1,5D-Korrektur.While in the known spin-stabilized artillery projectile with a reduction of the longitudinal rest thus a 1D correction, resulting in the artillery projectile according to the invention, a 1.5D correction.

Weitere Einzelheiten, Merkmale und Vorteile ergeben sich aus der nachfolgenden Beschreibung zweier in der Zeichnung verdeutlichter Ausführungsbeispiele des erfindungsgemäßen drallstabilisierten Artillerieprojektiles und seiner Wirkungsweise.Further details, features and advantages will become apparent from the following description of two illustrated in the drawings embodiments of the invention spin-stabilized artillery projectile and its mode of action.

Es zeigen:

Figur 1
abgeschnitten in einer Längsschnittdarstellung eine erste Ausbildung des Artillerieprojektiles,
Figur 2
eine der Figur 1 ähnliche Darstellung einer zweiten Ausführungsform des Artillerieprojektiles,
Figur 3
die Verbringung eines ballistisch gestarteten drallstabilisierten Artillerieprojektiles aus einem Geschütz in ein Zielgebiet, und
Figur 4
eine Draufsicht auf ein Zielgebiet, bei dem sowohl die Längsablage in der x-Richtung als auch die Querablage in der y-Richtung reduziert und folglich die Zielgenauigkeit entsprechend verbessert ist.
Show it:
FIG. 1
cut off in a longitudinal section a first formation of the artillery projectile,
FIG. 2
one of the FIG. 1 similar representation of a second embodiment of the artillery projectile,
FIG. 3
the transfer of a ballistic-launched spin-stabilized artillery projectile from a gun into a target area, and
FIG. 4
a plan view of a target area, in which reduced both the longitudinal shelf in the x-direction and the transverse shelf in the y-direction, and thus the target accuracy is improved accordingly.

Figur 1 zeigt längsgeschnitten den Vorderabschnitt einer Ausbildung des drallstabilisierten Artillerieprojektiles 10 mit einem in seiner Ogive 12 vorgesehenen Projektilzünder 14 und einer in der Ogive 12 vorgesehenen Bremseinrichtung 16, die fliehkraftbedingt durch pyrotechnische Kraftelemente 18 anstellbar ist, die einem vorderen Ringbereich 20 einer Haube 22 zugeordnet sind. FIG. 1 shows longitudinally sectioned the front portion of a formation of the spin-stabilized artillery projectile 10 with a provided in its ogive 12 projectile detonator 14 and a provided in the ogive 12 braking device 16 which is centrifugally force adjustable by pyrotechnic force elements 18, which are associated with a front ring portion 20 of a hood 22.

Die pyrotechnischen Kraftelemente 18 bilden Impulselemente 24 des Artillerieprojektiles 10, die am Umfang des Artillerieprojektiles 10 gleichmäßig verteilt angeordnet sind.The pyrotechnic force elements 18 form impulse elements 24 of the artillery projectile 10, which are arranged distributed uniformly on the circumference of the artillery projectile.

Die Bremseinrichtung 16 dient zur Reduktion der Längsablage des Artillerieprojektiles 10 in einem Zielgebiet (siehe die Figuren 3 und 4). In Figur 4 ist das Zielgebiet 26 ellipsenförmig, d.h. mit einem elliptischen Rand 28, verdeutlicht. Die durch den elliptischen Rand 28 begrenzte Ablagefläche 30 weist eine Längsachse A0 und eine Querachse B0 auf. Durch die Bremseinrichtung 16 ergibt sich eine Reduktion der Längsablage, d.h. der Längsachse A0, zu einem Betrag Ar. Eine Reduktion der Querachse B0 wird durch die Bremseinrichtung 16 des Artillerieprojektiles 10 nicht bewirkt, d.h. durch die Bremseinrichtung 16 wird die Ablagefläche 30 zu einer Ablagefläche 32 verkleinert, die durch die Randlinie 34 begrenzt ist.The braking device 16 serves to reduce the longitudinal storage of the artillery projectile 10 in a target area (see the Figures 3 and 4 ). In FIG. 4 is the target area 26 elliptical, ie with an elliptical edge 28, illustrated. The limited by the elliptical edge 28 shelf 30 has a longitudinal axis A 0 and a transverse axis B 0 . By the braking device 16 results in a reduction of the longitudinal shelf, ie the longitudinal axis A 0 , to an amount A r . A reduction of the transverse axis B 0 is not effected by the braking device 16 of the artillery projectile 10, ie by the braking device 16, the storage surface 30 is reduced to a storage surface 32 which is bounded by the edge line 34.

Mit Hilfe der am Umfang des Artillerieprojektiles 10 verteilten Impulselemente 24 ergibt sich durch passende Aktivierung der entsprechenden Impulselemente 24 bei einem Artillerieprojektil 10 mit Bremseinrichtung 16 eine Reduktion der Querablage des Artillerieprojektiles 10, d.h. eine weitere Reduktion der Ablagefläche 32 zu einer Ablagefläche 36, die durch die Randlinie 38 begrenzt ist. Die Ablagefläche 36 ist in x-Richtung durch die Längsabmessung Ar und in y-Richtung durch die Querabmessung Br bestimmt, wobei es bevorzugt ist, wenn Ar und Br gleich groß sind, so dass sich eine kreisrunde Ablagefläche 36 ergibt.With the help of the distributed on the circumference of the artillery projectile 10 pulse elements 24 is obtained by appropriate activation of the corresponding pulse elements 24 in an artillery projectile 10 with braking device 16, a reduction of the cross-stock of the artillery projectile 10, ie a further reduction of the storage surface 32 to a storage area 36 through the Edge line 38 is limited. The support surface 36 is determined in the x-direction by the longitudinal dimension A r and in the y-direction by the transverse dimension B r , wherein it is preferred if A r and B r are the same size, so that a circular support surface 36 results.

Bezüglich weiterer Einzelheiten des Artillerieprojektiles 10 gemäß Figur 1 wird auf die eingangs zitierte DE 101 43 312 C1 und DE 102 42 588 B4 Bezug genommen.For further details of the artillery projectile 10 according to FIG. 1 is on the cited above DE 101 43 312 C1 and DE 102 42 588 B4 Referenced.

Figur 2 verdeutlicht eine Ausbildung des Artillerieprojektiles 10 in einer der Figur 1 ähnlichen abgeschnittenen Längsschnittdarstellung, wobei die Impulselemente 24 an einem Ringelement 40 in Umfangsrichtung gleichmäßig verteilt vorgesehen sind, das zwischen dem Projektilzünder 14 und dem Projektilgehäuse 42 angeordnet ist. Die pyrotechnischen Kraftelemente 18 dienen bei dieser Ausführungsform des Artillerieprojektiles 10 nur zum Absprengen der die Bremseinrichtung 16 bedeckenden Haube 22. FIG. 2 clarifies a training of the artillery projectile 10 in one of FIG. 1 similar cutaway longitudinal sectional view, wherein the pulse elements 24 are provided on a ring member 40 in the circumferential direction uniformly distributed, the is arranged between the projectile fuze 14 and the projectile housing 42. The pyrotechnic force elements 18 are used in this embodiment of the artillery projectile 10 only for blowing off the brake device 16 covering the hood 22nd

Insbesondere bei Artillerieprojektilen 10 großer Reichweite 44 (siehe Figur 3) zwischen einem Ziel 46 und einem Geschütz 48, aus dem das Artillerieprojektil 10 abgefeuert wird, können die Impulselemente im Heckteil (Base Bleed) des Artillerieprojektiles 10 in Umfangsrichtung gleichmäßig verteilt vorgesehen sein.Especially with artillery projectiles 10 long range 44 (see FIG. 3 ) between a target 46 and a gun 48, from which the artillery projectile 10 is fired, the impulse elements in the rear part (base bleed) of the artillery projectile 10 may be distributed evenly in the circumferential direction.

In Figur 3 ist mit Bezugsziffer 50 ein Feuerleitrechner bezeichnet. Der Feuerleitrechner 50 bestimmt je nach der voraufgeklärten Richtung und Entfernung 44 von einem Geschütz 48 zu einem Ziel 46 die Azimutausrichtung, die durch den Doppelpfeil 52 angedeutete Elevation und die Treibladungsleistung, d.h. die theoretische Abgangsgeschwindigkeit 54 für die ballistische Bahnkurve 56 des Artillerieprojektiles 10 in das Zielgebiet 26.In FIG. 3 is designated reference numeral 50 a Feuerleitrechner. The fire control computer 50 determines the azimuth orientation, the elevation indicated by the double arrow 52, and the propellant power, ie, the theoretical exit velocity 54 for the ballistic trajectory 56 of the artillery projectile 10 into the target area, depending on the pre-enlightened direction and distance 44 from a gun 48 to a target 46 26th

Bezüglich der Reduktion der Längsablage des Artillerieprojektiles und des entsprechenden Verfahrens zur zielbezogenen Korrektur der ballistischen Flugbahn wird auf die eingangs zitierte EP 1 103 779 B1 Bezug genommen.With regard to the reduction of the longitudinal deposit of the artillery projectile and the corresponding method for target-related correction of the ballistic trajectory is cited at the outset EP 1 103 779 B1 Referenced.

Bezugsziffernliste:List of reference numerals:

1010
Artillerieprojektilartillery projectile
1212
Ogive (von 10)Ogive (out of 10)
1414
Projektilzünder (in 12)Projectile fuse (in 12)
1616
Bremseinrichtung (von 10)Braking device (from 10)
1818
pyrotechnische Kraftelemente (für 20)pyrotechnic force elements (for 20)
2020
vorderer Ringbereich (von 22)front ring area (from 22)
2222
Haube (für 16)Hood (for 16)
2424
Impulselemente (von 10)Impulse elements (of 10)
2626
Zielgebiet (von 10 bei 46)Target area (from 10 at 46)
2828
elliptischer Rand (von 30)elliptical edge (from 30)
3030
Ablageflächeshelf
3232
1 D-reduzierte Ablagefläche1 D-reduced shelf
3434
Randlinie (von 32)Edge line (from 32)
3636
1,5D-reduzierte Ablagefläche1.5D reduced storage space
3838
Randlinie (von 36)Border line (from 36)
4040
Ringelement (zwischen 14 und 42 für 24)Ring element (between 14 and 42 for 24)
4242
Projektilgehäuse (von 10)Projectile housing (from 10)
4444
Reichweite (von 10 zwischen 48 und 46)Range (from 10 between 48 and 46)
4646
Zielaim
4848
Geschütz (für 10)Gun (for 10)
5050
Feuerleitrechner (für 48)Fire control computer (for 48)
5252
Doppelpfeil/Elevation (von 48)Double Arrow / Elevation (from 48)
5454
Abgangsgeschwindigkeit (von 10)Leaving speed (of 10)
5656
Ballistische Bahnkurve (von 10 zwischen 48 und 26)Ballistic trajectory (from 10 between 48 and 26)

Claims (4)

  1. Spin-stabilized artillery projectile (10) with a projectile detonator (14) provided in its ogive (12) and a radially deployed brake device (16) provided in the ogive (12) for reduction of the longitudinal offset (A0; Ar) of the artillery projectile (10) in a target area (26),
    characterized in that
    a) the artillery projectile (10) has a number of impulse elements (24) distributed around its circumference that are provided to reduce the lateral offset (B0; Br) of the artillery projectile (10) in the target area (26),
    b) in which case an impulse element (24), which matches the reduction in the lateral offset (B0; Br) can be activated deliberately via a device which interacts with the impulse elements (24) and by means of which the respective instantaneous rotation angle position of the artillery projectile (10), and therefore of the impulse elements (24), which are separated from one another in the circumferential direction, can be determined, and
    c) in which case the impulse elements (24) are provided on a ring element (40), which is arranged between the projectile fuze (14) and the projectile casing (42).
  2. Artillery projectile (10) according to Claim 1,
    characterized in that
    the impulse elements (24) are evenly distributed around the circumference of the ring element (40).
  3. Artillery projectile (10) according to Claim 1 or 2,
    characterized in that
    the device is provided in the artillery projectile (10).
  4. Artillery projectile (10) according to one of the preceding claims,
    characterized in that
    the device is controlled with the aid of a satellite.
EP06022695A 2005-11-03 2006-10-31 Spin-stabilised artillery projectile Not-in-force EP1783451B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102005052474A DE102005052474B3 (en) 2005-11-03 2005-11-03 Spiked artillery projectile

Publications (3)

Publication Number Publication Date
EP1783451A2 EP1783451A2 (en) 2007-05-09
EP1783451A3 EP1783451A3 (en) 2007-08-29
EP1783451B1 true EP1783451B1 (en) 2008-12-17

Family

ID=37697820

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06022695A Not-in-force EP1783451B1 (en) 2005-11-03 2006-10-31 Spin-stabilised artillery projectile

Country Status (5)

Country Link
US (1) US7360490B2 (en)
EP (1) EP1783451B1 (en)
AT (1) ATE418059T1 (en)
DE (2) DE102005052474B3 (en)
ES (1) ES2317401T3 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3035205B1 (en) * 2015-04-20 2018-10-05 Roxel France DEVICE FOR CORRECTING THE TRACK OF A PROJECTILE AND METHOD OF CORRECTING A TRACK
CN115358638A (en) * 2022-10-19 2022-11-18 中国兵器科学研究院 Fire distribution method and device, electronic equipment and storage medium

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2809281C2 (en) * 1978-03-03 1984-01-05 Emile Jean Versailles Stauff Control device for a self-rotating projectile
DE3546269C1 (en) * 1985-12-28 1987-08-13 Deutsche Forsch Luft Raumfahrt Missile
FR2686687B1 (en) * 1987-04-22 1994-05-13 Thomson Brandt Armements METHOD AND DEVICE FOR DRIVING A PROJECTILE ACCORDING TO ITS THREE AXES OF ROLL TANGAGE AND LACE.
EP0418636B1 (en) 1989-09-19 1993-12-29 DIEHL GMBH & CO. Projectile with trajectory control system
DE4036166A1 (en) * 1990-11-14 1992-05-21 Diehl Gmbh & Co RAILWAY CORRECTABLE PROJECT
US5456429A (en) 1993-08-02 1995-10-10 Loral Corp. Thrust maneuver system
US5647558A (en) * 1995-02-14 1997-07-15 Bofors Ab Method and apparatus for radial thrust trajectory correction of a ballistic projectile
DE19957363A1 (en) 1999-11-29 2001-05-31 Diehl Munitionssysteme Gmbh Procedure for correcting a ballistic trajectory
DE10242588B4 (en) * 2001-09-04 2005-06-30 Diehl Bgt Defence Gmbh & Co. Kg Braking device for a web-corrected spin-stabilized artillery projectile
DE10143312C1 (en) 2001-09-04 2003-06-18 Diehl Munitionssysteme Gmbh Braking device for a path-correctable spin-stabilized artillery projectile
EP1540264B1 (en) 2002-09-13 2010-06-09 Diehl BGT Defence GmbH & Co.KG Braking device for a trajectory-correctable spin-stabilized artillery projectile
US7121210B2 (en) * 2003-02-18 2006-10-17 Kdi Precision Products, Inc. Accuracy fuze for airburst cargo delivery projectiles

Also Published As

Publication number Publication date
ATE418059T1 (en) 2009-01-15
EP1783451A3 (en) 2007-08-29
DE502006002369D1 (en) 2009-01-29
DE102005052474B3 (en) 2007-07-12
ES2317401T3 (en) 2009-04-16
EP1783451A2 (en) 2007-05-09
US7360490B2 (en) 2008-04-22
US20070095238A1 (en) 2007-05-03

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