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EP0288721B1 - Provision for a breaking line at the aft part of the sabot of a sub-calibre type projectile - Google Patents

Provision for a breaking line at the aft part of the sabot of a sub-calibre type projectile Download PDF

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Publication number
EP0288721B1
EP0288721B1 EP88104229A EP88104229A EP0288721B1 EP 0288721 B1 EP0288721 B1 EP 0288721B1 EP 88104229 A EP88104229 A EP 88104229A EP 88104229 A EP88104229 A EP 88104229A EP 0288721 B1 EP0288721 B1 EP 0288721B1
Authority
EP
European Patent Office
Prior art keywords
sabot
projectile
provision
breaking line
projectile body
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
EP88104229A
Other languages
German (de)
French (fr)
Other versions
EP0288721A1 (en
Inventor
Jakob Burri
Rudolf Rossmann
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 Air Defence AG
Original Assignee
Werkzeugmaschinenfabrik Oerlikon Buhrle AG
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 Werkzeugmaschinenfabrik Oerlikon Buhrle AG filed Critical Werkzeugmaschinenfabrik Oerlikon Buhrle AG
Publication of EP0288721A1 publication Critical patent/EP0288721A1/en
Application granted granted Critical
Publication of EP0288721B1 publication Critical patent/EP0288721B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B14/00—Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
    • F42B14/06—Sub-calibre projectiles having sabots; Sabots therefor
    • F42B14/064—Sabots enclosing the rear end of a kinetic energy projectile, i.e. having a closed disk shaped obturator base and petals extending forward from said base

Definitions

  • the invention relates to the formation of a predetermined breaking point on the rear part of a sabot according to the preamble of the claim.
  • EP-A-0 131 073 discloses a detaching device for a nozzle-driven projectile, in which the projectile or a missile is held over a fusible connecting part.
  • the fusible connecting part has an annular part which is weakened by a circumferential groove and in which a multiplicity of through openings for the hot exhaust gases are additionally uniformly provided on the circumference.
  • the exact detachment of the rocket is now determined by the choice of the meltable material for the connecting part and the dimensioning of the groove and the through openings, ie detachment takes place via the melting effect of the hot exhaust gases.
  • the object which is to be achieved with the present invention consists in the creation or formation of a predetermined breaking point which breaks reliably in the desired manner and at the desired point in time without influencing the flight stability of the projectile core.
  • this predetermined breaking point is characterized by claim 1.
  • the sabot projectile has a projectile body 10, a sabot rear part 11 and a sabot jacket 12.
  • a ballistic hood 13 is fastened on the projectile body 10.
  • a hard metal alloy preferably a tungsten alloy
  • the sabot rear part 11 is preferably made of light metal and the sabot jacket 12 made of plastic.
  • the sabot jacket 12 usually consists of three segments which are connected to one another with the aid of suitable predetermined breaking points 14. 1 shows only a single predetermined breaking point 14.
  • the sabot jacket 12 has cutouts 15 and a guide band 16.
  • the projectile body 10 has two circumferential grooves 17 which are used to fasten the sabot rear part 11 to the projectile body 10.
  • This sabot rear part 11 has six tongues 18 which protrude with projections 25 into the circumferential grooves 17 of the projectile body 10.
  • the sabot rear part 11 can separate from the projectile body 10 when the sabot projectile emerges from the weapon barrel, there is an inner groove 29 on the sabot rear part 11, through which a predetermined breaking point is formed, at which the tongues 18 can be broken off from the sabot rear part 11.
  • the six tongues 18 are separated from one another by six slots 30. Thanks to the groove 29 shown in FIG. 2 and thanks to the slots 30 between the tongues 18, after the sabot projectile has left the weapon barrel, the six tongues 18 can bend as far outwards under the effect of the centrifugal force generated by the swirl, that they break off and therefore not the projectile body 10 hold more with their cams 25 in the circumferential grooves 17.
  • a further, outer circumferential groove 31 is provided on the sabot rear part 11, the wall thickness between the two grooves 29 and 31 being chosen to be just thick enough that the tongues 18 can be easily broken out by the centrifugal force.
  • a disc-shaped recess 32 is provided on each tongue 18, see also FIG. 3.
  • two rectangular recesses 33 are pressed into the base of the disk-shaped recesses 32, whereby the cams 25 are formed, by which the projectile body 10 is held in the sabot rear part 11, since these cams 25 into the Protrude grooves 17 into it.
  • the sabot rear part 11 also has a further circumferential groove 34, which is used for fastening a cartridge case, not shown in the drawing.
  • the sabot rear part 11 has a circumferential sealing groove 19 and a circumferential retaining groove 26.
  • This circumferential sealing groove has mutually parallel side walls 21, 22, these mutually parallel side walls 21, 22 being inclined forward by an angle of approximately 75 ° with respect to the longitudinal axis of the weapon.
  • the circumferential retaining groove has two side walls 24 and 28, of which one side wall 24 is inclined rearward by 75 ° and the other side wall 28 is inclined forward by 75 °.
  • the circumferential retaining groove 26 and the circumferential sealing groove 19 are separated from one another by a rib 23.
  • the predetermined breaking point between the two circumferential grooves 29 and 31 is now supplemented by bores 40.
  • These holes 40 are shown in all Figures 1-3. Either there can be a single hole 40 per tongue 18 near one of the two slots 30, or there can be two holes 40 per tongue 18, one hole 40 near one slot 30 and the other Bore 40 is located near the other slot 30.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Drilling And Exploitation, And Mining Machines And Methods (AREA)
  • Toys (AREA)
  • Rear-View Mirror Devices That Are Mounted On The Exterior Of The Vehicle (AREA)
  • Mirrors, Picture Frames, Photograph Stands, And Related Fastening Devices (AREA)
  • Road Signs Or Road Markings (AREA)

Description

Die Erfindung betrifft die Ausbildung einer Sollbruchstelle am Heckteil eines Treibspiegels gemäss dem Oberbegriff des Patentanspruches.The invention relates to the formation of a predetermined breaking point on the rear part of a sabot according to the preamble of the claim.

Treibspiegelgeschosse dieser Art gehören zum Stande der Technik, es wird beispielsweise auf folgende Patentschriften hingewiesen:
   US-PS 3 927 618 und 4 249 466
   CH-PS 494 389 und 536 481
   GB-PS 576 217 und 1 362 308This type of sabot projectile belongs to the state of the art; reference is made, for example, to the following patents:
U.S. Patent Nos. 3,927,618 and 4,249,466
CH-PS 494 389 and 536 481
GB-PS 576 217 and 1 362 308

Insbesondere bei Treibspiegelgeschossen gemäss der EP-A-0 072 584, welche den nächstliegenden Stand der Technik bildet, hat es sich gezeigt, dass die am Treibspiegelheck befestigten Zungen nicht immer in der gewünschten Weise an der Sollbruchstelle abbrechen. Falls sich nun der gesamte Treibspiegel und insbesondere das Treibspiegelheck nicht in der gewünschten Weise vom Geschosskern - sofort beim Verlassen der Rohrmündung - ablöst, dann ist der stabile Flug des Geschosskernes nicht mehr gewährleistet.Particularly in the case of sabot projectiles according to EP-A-0 072 584, which forms the closest prior art, it has been shown that the tongues attached to the sabot tail do not always break off at the predetermined breaking point in the desired manner. If the entire sabot and especially the sabot tail does not detach itself from the projectile core in the desired manner - immediately upon leaving the pipe muzzle - then the stable flight of the projectile core is no longer guaranteed.

Ferner ist aus der EP-A-0 131 073 eine Ablösevorrichtung für ein düsenangetriebenes Geschoss bekannt, bei der das Geschoss bzw. eine Rakete über einen schmelzbaren Verbindungsteil gehalten wird. Der schmelzbare Verbindungsteil weist einen ringförmigen Teil auf, welcher durch eine Umfangsnut geschwächt ist und in der zusätzlich eine Vielzahl von Durchgangsöffnungen für die heissen Abgase gleichmässig am Umfang angebracht sind. Das exakte Ablösen der Rakete wird nun bestimmt durch die Wahl des schmelzbaren Materials für den Verbindungsteil und der Dimensionierung der Nut und der Durchgangsöffnungen, d.h. das Ablösen erfolgt über die Schmelzwirkung der heissen Abgase.Furthermore, EP-A-0 131 073 discloses a detaching device for a nozzle-driven projectile, in which the projectile or a missile is held over a fusible connecting part. The fusible connecting part has an annular part which is weakened by a circumferential groove and in which a multiplicity of through openings for the hot exhaust gases are additionally uniformly provided on the circumference. The exact detachment of the rocket is now determined by the choice of the meltable material for the connecting part and the dimensioning of the groove and the through openings, ie detachment takes place via the melting effect of the hot exhaust gases.

Die Aufgabe, welche mit der vorliegenden Erfindung gelöst werden soll, besteht in der Schaffung oder Ausbildung einer Sollbruchstelle, welche zuverlässig in der gewünschten Art und Weise und zum gewünschten Zeitpunkt bricht, ohne die Flugstabilität des Geschosskernes zu beeinflussen.The object which is to be achieved with the present invention consists in the creation or formation of a predetermined breaking point which breaks reliably in the desired manner and at the desired point in time without influencing the flight stability of the projectile core.

Erfindungsgemäss ist diese Sollbruchstelle durch den Anspruch 1 gekennzeichnet.According to the invention, this predetermined breaking point is characterized by claim 1.

Diese Ausbildung der Sollbruchstelle hat folgende Vorteile:

  • a) Es wird vermieden, dass das Treibspiegelheck zerbricht, statt dass die einzelnen Zungen abbrechen.
  • b) Die Wurzelpartie der Zungen, d.h. die Stelle, an der sie abbrechen sollen, kann steifer ausgebildet werden.
  • c) Schwankungen in der Qualität des Werkstoffes haben weniger Bedeutung.
  • d) Die Gefahr der unerwünschten Rissbildung im Treibspiegelheck wird vermindert.
This design of the predetermined breaking point has the following advantages:
  • a) It is avoided that the sabot rear end breaks, instead of the individual tongues breaking off.
  • b) The root part of the tongues, ie the point at which they should break off, can be made stiffer.
  • c) Fluctuations in the quality of the material have less importance.
  • d) The risk of undesirable crack formation in the sabot rear is reduced.

Es kann sich aber auch zu beiden Seiten der Zunge je eine Bohrung befinden.But there can also be a hole on both sides of the tongue.

Ein Ausführungsbeispiel des Treibspiegelgeschosses mit der erfindungsgemäss ausgebildeten Sollbruchstelle ist im folgenden anhand der beigefügten Zeichnung ausführlich beschrieben. Es zeigt:

Fig.1
einen Längsschnitt durch ein Treibspiegelgeschoss mit der erfindungsgemässen Ausbildung der Sollbruchstelle,
Fig.2
in vergrössertem Massstab das Treibspiegelheckteil des in Fig.1 dargestellten Treibspiegelgeschosses,
Fig.3
eine perspektivische Darstellung des in Fig.2 dargestellten Treibspiegelheckteils.
An embodiment of the sabot projectile with the predetermined breaking point designed according to the invention is described in detail below with reference to the accompanying drawing. It shows:
Fig. 1
2 shows a longitudinal section through a sabot projectile with the design of the predetermined breaking point according to the invention,
Fig. 2
on an enlarged scale the sabot rear part of the sabot projectile shown in FIG. 1,
Fig. 3
a perspective view of the sabot rear part shown in Figure 2.

Gemäss Fig.1 weist das Treibspiegelgeschoss einen Geschosskörper 10, einen Treibspiegelheckteil 11 und einen Treibspiegelmantel 12 auf. Auf dem Geschosskörper 10 ist eine ballistische Haube 13 befestigt. Vorzugsweise wird für die Herstellung des Geschosskörpers 10 eine Hartmetallegierung, vorzugsweise eine Wolframlegierung, verwendet, die für solche Geschosse wohl bekannt ist. Der Treibspiegelheckteil 11 wird vorzugsweise aus Leichtmetall hergestellt und der Treibspiegelmantel 12 aus Kunststoff. Der Treibspiegelmantel 12 besteht üblicherweise aus drei Segmenten, die miteinander mit Hilfe von geeigneten Sollbruchstellen 14 verbunden sind. In Fig.1 ist nur eine einzige Sollbruchstelle 14 dargestellt. Ausserdem weist der Treibspiegelmantel 12 Aussparungen 15 und ein Führungsband 16 auf. Der Geschosskörper 10 besitzt zwei Umfangsnuten 17, die zur Befestigung des Treibspiegelheckteiles 11 am Geschosskörper 10 dienen. Dieser Treibspiegelheckteil 11 weist sechs Zungen 18 auf, welche mit Vorsprüngen 25 in die Umfangsnuten 17 des Geschosskörpers 10 hineinragen.According to FIG. 1, the sabot projectile has a projectile body 10, a sabot rear part 11 and a sabot jacket 12. A ballistic hood 13 is fastened on the projectile body 10. Preferably, a hard metal alloy, preferably a tungsten alloy, is used for the manufacture of the projectile body 10, which is well known for such projectiles. The sabot rear part 11 is preferably made of light metal and the sabot jacket 12 made of plastic. The sabot jacket 12 usually consists of three segments which are connected to one another with the aid of suitable predetermined breaking points 14. 1 shows only a single predetermined breaking point 14. In addition, the sabot jacket 12 has cutouts 15 and a guide band 16. The projectile body 10 has two circumferential grooves 17 which are used to fasten the sabot rear part 11 to the projectile body 10. This sabot rear part 11 has six tongues 18 which protrude with projections 25 into the circumferential grooves 17 of the projectile body 10.

Damit sich beim Austritt des Treibspiegelgeschosses aus dem Waffenrohr der Treibspiegelheckteil 11 vom Geschosskörper 10 trennen kann, ist eine innere Nut 29 am Treibspiegelheckteil 11 vorhanden, durch welche eine Sollbruchstelle gebildet wird, an welcher die Zungen 18 vom Treibspiegelheckteil 11 abgebrochen werden können. Wie insbesondere aus Fig.3 ersichtlich ist, sind die sechs Zungen 18 durch sechs Schlitze 30 voneiander getrennt. Dank der in Fig.2 dargestellten Nut 29 und dank der Schlitze 30 zwischen den Zungen 18, können sich, nachdem das Treibspiegelgeschoss das Waffenrohr verlassen hat, die sechs Zungen 18 unter der Wirkung der durch den Drall erzeugten Fliehkraft, so weit nach aussen biegen, dass sie abbrechen und somit den Geschosskörper 10 nicht mehr mit ihren Nocken 25 in den Umfangsnuten 17 festhalten. Zur Erleichterung dieser Freigabe des Geschosskörpers 10 ist am Treibspiegelheckteil 11 noch eine weitere, äussere Umfangsnut 31 vorhanden, wobei die Wandstärke zwischen den beiden Nuten 29 und 31 gerade so dick gewählt ist, dass sich die Zungen 18 durch die Fliehkraft leicht herausbrechen lassen.So that the sabot rear part 11 can separate from the projectile body 10 when the sabot projectile emerges from the weapon barrel, there is an inner groove 29 on the sabot rear part 11, through which a predetermined breaking point is formed, at which the tongues 18 can be broken off from the sabot rear part 11. As can be seen in particular from FIG. 3, the six tongues 18 are separated from one another by six slots 30. Thanks to the groove 29 shown in FIG. 2 and thanks to the slots 30 between the tongues 18, after the sabot projectile has left the weapon barrel, the six tongues 18 can bend as far outwards under the effect of the centrifugal force generated by the swirl, that they break off and therefore not the projectile body 10 hold more with their cams 25 in the circumferential grooves 17. To facilitate this release of the projectile body 10, a further, outer circumferential groove 31 is provided on the sabot rear part 11, the wall thickness between the two grooves 29 and 31 being chosen to be just thick enough that the tongues 18 can be easily broken out by the centrifugal force.

Zur Herstellung der Nocken 25, die ja erst nach dem Einsetzen des Geschosskörpers 10 in den Treibspiegelheckteil 11 erzeugt werden dürfen, ist an jeder Zunge 18 eine scheibenförmige Aussparung 32 vorhanden, siehe auch Fig.3. Sobald der Geschosskörper 10 in den Treibspiegelheckteil 11 eingesetzt worden ist, werden in den Grund der scheibenförmigen Aussparungen 32 je zwei rechteckige Aussparungen 33 hineingepresst, wodurch die Nocken 25 entstehen, durch welche der Geschosskörper 10 im Treibspiegelheckteil 11 gehalten wird, da diese Nocken 25 in die Nuten 17 hinein ragen.For the production of the cams 25, which may only be produced after the projectile body 10 has been inserted into the sabot rear part 11, a disc-shaped recess 32 is provided on each tongue 18, see also FIG. 3. As soon as the projectile body 10 has been inserted into the sabot rear part 11, two rectangular recesses 33 are pressed into the base of the disk-shaped recesses 32, whereby the cams 25 are formed, by which the projectile body 10 is held in the sabot rear part 11, since these cams 25 into the Protrude grooves 17 into it.

Ausserdem weist der Treibspiegelheckteil 11 noch eine weitere Umfangsnut 34 auf, die zur Befestigung einer in der Zeichnung nicht dargestellten Patronenhülse dient.In addition, the sabot rear part 11 also has a further circumferential groove 34, which is used for fastening a cartridge case, not shown in the drawing.

Gemäss Fig.2 weist der Treibspiegelheckteil 11 eine Umfangsdichtungsnut 19 und eine Umfangshaltenut 26 auf. Diese Umfangsdichtungsnut hat zueinander parallele Seitenwände 21,22, wobei diese zueinander parallelen Seitenwände 21,22 um einen Winkel von etwa 75° nach vorne, bezüglich der Waffenlängsachse geneigt sind. Die Umfangshaltenut hat gemäss Fig.2 zwei Seitenwände 24 und 28, von denen die eine Seitenwand 24 um 75° nach hinten geneigt ist und die andere Seitenwand 28 um 75° nach vorne geneigt ist. Die Umfangshaltenut 26 und die Umfangsdichtungsnut 19 sind durch eine Rippe 23 voneinander getrennt.According to FIG. 2, the sabot rear part 11 has a circumferential sealing groove 19 and a circumferential retaining groove 26. This circumferential sealing groove has mutually parallel side walls 21, 22, these mutually parallel side walls 21, 22 being inclined forward by an angle of approximately 75 ° with respect to the longitudinal axis of the weapon. According to FIG. 2, the circumferential retaining groove has two side walls 24 and 28, of which one side wall 24 is inclined rearward by 75 ° and the other side wall 28 is inclined forward by 75 °. The circumferential retaining groove 26 and the circumferential sealing groove 19 are separated from one another by a rib 23.

Erfindungsgemäss wird nun die Sollbruchstelle zwischen den beiden Umfangsnuten 29 und 31 durch Bohrungen 40 ergänzt. Diese Bohrungen 40 sind in allen Figuren 1-3 dargestellt. Es kann entweder pro Zunge 18 eine einzige Bohrung 40 in der Nähe einer der beiden Schlitze 30 vorhanden sein, oder es können pro Zunge 18 je zwei Bohrungen 40 vorhanden sein, wobei sich die eine Bohrung 40 in der Nähe des einen Schlitzes 30 und die andere Bohrung 40 in der Nähe des anderen Schlitzes 30 befindet.According to the invention, the predetermined breaking point between the two circumferential grooves 29 and 31 is now supplemented by bores 40. These holes 40 are shown in all Figures 1-3. Either there can be a single hole 40 per tongue 18 near one of the two slots 30, or there can be two holes 40 per tongue 18, one hole 40 near one slot 30 and the other Bore 40 is located near the other slot 30.

Durch diese beiden Bohrungen 40 bzw. durch eine einzige Bohrung 40 wird die Rissbildung gefördert, sodass die Zungen 18 leichter abbrechen, ohne dass die Wandstärke zwischen den beiden Umfangsnuten 29 und 31 vermindert werden muss.Crack formation is promoted through these two bores 40 or through a single bore 40, so that the tongues 18 break off more easily without the wall thickness between the two circumferential grooves 29 and 31 having to be reduced.

Claims (2)

  1. Provision of a breaking line on the aft section of a sabot for a sabot projectile, comprising
    - a projectile body (10̸) or penetrator,
    - a sabot aft section (11) into which the projectile body (10̸) is anchored,
    - a sabot casing (12) which encases the projectile body (10̸),
    - a number of tongues (18), which are attached to the sabot aft section (11) by way of breaking lines (29, 31), for anchoring the projectile body (10̸) in the sabot aft section (11), wherein the breaking lines (29, 31) are formed by two peripheral grooves (29, 31),
    characterised in that each breaking line (29, 31) comprises a bore (40̸) which extends from the one peripheral groove (29) to the other peripheral groove (31) and which is located on one side of the tongue (18).
  2. Provision of a breaking line according to claim 1, characterised in that a respective bore (40̸) is provided on both sides of the tongue (18).
EP88104229A 1987-04-30 1988-03-17 Provision for a breaking line at the aft part of the sabot of a sub-calibre type projectile Expired - Lifetime EP0288721B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH1634/87 1987-04-30
CH163487 1987-04-30

Publications (2)

Publication Number Publication Date
EP0288721A1 EP0288721A1 (en) 1988-11-02
EP0288721B1 true EP0288721B1 (en) 1993-09-22

Family

ID=4215039

Family Applications (1)

Application Number Title Priority Date Filing Date
EP88104229A Expired - Lifetime EP0288721B1 (en) 1987-04-30 1988-03-17 Provision for a breaking line at the aft part of the sabot of a sub-calibre type projectile

Country Status (8)

Country Link
US (1) US4776280A (en)
EP (1) EP0288721B1 (en)
JP (1) JPS63282500A (en)
CA (1) CA1312778C (en)
DE (1) DE3884257D1 (en)
IL (1) IL86048A (en)
NO (1) NO163425C (en)
ZA (1) ZA882945B (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3724401A1 (en) * 1987-07-23 1989-05-18 Rheinmetall Gmbh Wing-stabilized, sub-caliber floating cage
US4881466A (en) * 1988-12-23 1989-11-21 General Electric Company High velocity sabot for spin stabilized penetrator
FR2642161B1 (en) * 1989-01-26 1991-04-26 France Etat Armement UNDER CALIBER PROJECTILE AND METHOD FOR MOUNTING AND FIXING A SHELL BODY IN AN UNDER CALIBER PROJECTILE
FR2665761B1 (en) * 1990-08-13 1994-09-16 Giat Ind Sa SEALING BELT FOR ARROW PROJECTILE.
EG21731A (en) * 1993-09-24 2002-02-27 Contraves Pyrotec Ag Releasable sabot for a subcaliber projectile
DE19650741C2 (en) * 1996-12-06 1999-11-11 Rheinmetall W & M Gmbh Process for the manufacture of a sub-caliber projectile
FR2768809B1 (en) * 1997-09-24 1999-10-15 Giat Ind Sa LARGE CALIBER LONG RANGE FIELD ARTILLERY PROJECTILE
US6564720B1 (en) * 2000-01-14 2003-05-20 Olin Corporation Sabot for a bullet
DE102010045474A1 (en) * 2010-09-16 2012-03-22 Rheinmetall Waffe Munition Gmbh Projectile with disposable sabot
KR101527434B1 (en) * 2015-01-08 2015-06-10 주식회사 풍산 Spin stabilized projectile formed with non-slip squeezing groove and saw tooth
DE102020115703B4 (en) * 2020-06-15 2024-02-22 Rheinmetall Waffe Munition Gmbh sabot

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB576217A (en) * 1943-03-08 1946-03-25 Ladislas Permutter Improvements in projectiles
NL137889C (en) * 1967-07-28
CH536481A (en) * 1971-03-29 1973-06-15 Oerlikon Buehrle Ag Sabot bullet and process for its manufacture
US3927618A (en) * 1971-03-29 1975-12-23 Oerlikon Buehrle Ag Sabot projectile
DE2223477A1 (en) * 1972-05-13 1973-11-22 Paul J Kopsch Shell antifriction coating - for a shell with a disengaging lightweight cap
CH622883A5 (en) * 1977-07-21 1981-04-30 Oerlikon Buehrle Ag
US4403435A (en) * 1981-04-02 1983-09-13 Brunswick Corporation Release and alignment mechanism for jet-propelled projectiles
DE3261947D1 (en) * 1981-08-13 1985-02-28 Oerlikon Buehrle Ag Connection between the casing and the rear part of a sabot for a projectile
EP0236705B1 (en) * 1986-03-07 1989-11-29 Werkzeugmaschinenfabrik Oerlikon-Bührle AG Connection between the casing and the bottom of a sabot for a subcalibre projectile

Also Published As

Publication number Publication date
CA1312778C (en) 1993-01-19
NO163425C (en) 1990-05-23
NO881142L (en) 1988-10-31
NO881142D0 (en) 1988-03-15
DE3884257D1 (en) 1993-10-28
JPS63282500A (en) 1988-11-18
IL86048A0 (en) 1988-09-30
NO163425B (en) 1990-02-12
IL86048A (en) 1992-09-06
US4776280A (en) 1988-10-11
EP0288721A1 (en) 1988-11-02
ZA882945B (en) 1988-12-28

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