FR2573681A1 - COMBAT HEAD OF A LARGE SIZE PROJECTILE OR A ROCKET - Google Patents

COMBAT HEAD OF A LARGE SIZE PROJECTILE OR A ROCKET Download PDF

Info

Publication number
FR2573681A1
FR2573681A1 FR8515870A FR8515870A FR2573681A1 FR 2573681 A1 FR2573681 A1 FR 2573681A1 FR 8515870 A FR8515870 A FR 8515870A FR 8515870 A FR8515870 A FR 8515870A FR 2573681 A1 FR2573681 A1 FR 2573681A1
Authority
FR
France
Prior art keywords
rocket
head
combat head
combat
large size
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.)
Pending
Application number
FR8515870A
Other languages
French (fr)
Inventor
Erich Bock
Rainer Himmert
Martin Seehofer
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 FR2573681A1 publication Critical patent/FR2573681A1/en
Pending 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
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/72—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
    • F42B12/76—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the casing

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

L'INVENTION CONCERNE UNE ENVELOPPE DE TETE DE COMBAT EN DEUX PARTIES, COMPRENANT UNE SECTION EN OGIVE 4 ET UNE SECTION CYLINDRIQUE 10. SELON L'INVENTION, CETTE ENVELOPPE DE TETE DE COMBAT EST REALISEE D'UN SEUL TENANT PAR FLUAGE SOUS PRESSION EN ACIER AU CARBONE.THE INVENTION RELATED TO A TWO-PART COMBAT HEAD ENCLOSURE, INCLUDING A 4-OGIVE SECTION AND A 10 CYLINDRICAL SECTION. ACCORDING TO THE INVENTION, THIS COMBAT HEAD ENCLOSURE IS MADE FROM A SINGLE TENSION BY PRESSURE CREEPING OF STEEL CARBON.

Description

Tête de combat d'un projectile à gros calibre ou d'une fusée La présenteCombat head of a large caliber projectile or rocket

invention concerne une tête de combat d'un projectile à gros calibre ou d'une fusée, comprenant une partie en ogive et une partie cylindrique qui lui est reliée, le rapport du diamètre extérieur à la longueur totale étant d'environ 1: 4 à 1:10 On connaît, par la DE-B 11 84 674, un projectile  The invention relates to a combat head of a large caliber projectile or rocket, comprising an ogival portion and a cylindrical portion connected thereto, the ratio of outer diameter to total length being from about 1: 4 to about 1:10 DE-B 11 84 674 discloses a projectile

muni d'une charge utile, constituée notamment par des feuil-  equipped with a payload, consisting in particular of

les volantes. Ce projectile en forme de fusée comporte une tête de combat en deux parties, comprenant une tête en ogive et une section cylindrique contenant la charge utile qui lui est reliée. Ces deux parties sont reliées entre elles par une tige axiale ou un tube axial. Pour cela, on prévoit une tête et un fond correspondants coportan-t des f îletaaes qui sont reliés entre eux par la tige axiale. Ainsi, le coût  the flying ones. This rocket-shaped projectile has a two-part combat head comprising a warhead and a cylindrical section containing the payload connected thereto. These two parts are interconnected by an axial rod or an axial tube. For this purpose, a corresponding head and bottom are provided which are connected to each other by the axial rod. So the cost

de fabrication d'une telle tête de combat est très élevé.  manufacturing such a fighting head is very high.

L'invention a pour objet une tête de combat beaucoup  The subject of the invention is a combat head

moins coûteuse.less expensive.

Pour atteindre cet objectif, selon l'invention, l'enveloppe (1) de la tête d'attaque est réalisée d'un seul tenant et est constituée par une matière pouvant être usinée  To achieve this objective, according to the invention, the envelope (1) of the drive head is made in one piece and is constituted by a material that can be machined

par fluage sous pression telle que de l'acier au carbone.  by creep under pressure such as carbon steel.

L'un des avantages de l'invention consiste en ce que, non seulement le coût de production est réduit, mais l'on obtient également une économie de poids considérable, du fait qu'on n'a plus besoin des pièces de raccordement  One of the advantages of the invention is that, not only is the cost of production reduced, but a considerable saving in weight is also achieved, since connection pieces are no longer needed.

antérieurement nécessaires.previously necessary.

Selon un mode de réalisation de l'invention, on  According to one embodiment of the invention,

prévoit une partie d'embouchure épaissie comportant un tarau-  provides for a thickened mouthpiece with a

dage. Cela permet de visser directement une fusée d'amorçage  dage. This makes it possible to directly screw a priming rocket

dans la tête, sans avoir à faire appel à des pièces de rac-  in the head, without having to resort to

cordement correspondantes. Cela permet également des économies  corresponding string. It also saves money

de coût et de poids.cost and weight.

Selon un autre mode de réalisation de l'invention,  According to another embodiment of the invention,

l'épaisseur de paroi est constante jusqu'à la partie d'embou-  the wall thickness is constant up to the embossing portion

chure. Ainsi, la tête présente en son intérieur une surface continue, permettant un degré de remplissage élevé en ce  chure. Thus, the head has in its interior a continuous surface, allowing a high degree of filling in this

qui concerne une charge utile.which concerns a payload.

Un point essentiel pour l'invention consiste en  An essential point for the invention consists in

ce que la tête est d'un maniement sûr en raison de sa con-  that the head is safe to use because of its

formation en une seule pièce, du fait qu'il n'y a pas de  one-piece training, because there is no

zone de séparation (comme dans l'état actuel de la techni-  separation zone (as in the current state of the art

que). Les vices de fabrication et de montage inhérants à  than). Manufacturing and assembly defects inherent in

ces systèmes sont également supprimés.  these systems are also removed.

On va décrire à présent un exemple de réalisation  We will now describe an example of realization

de l'invention représenté sur le dessin annexé.  of the invention shown in the accompanying drawing.

Une enveloppe 1 de tête de combat d'une fusée non représentée présente une longueur toale 2 pour un diamètre 3 d'une partie cylindrique 4. Le rapport du diamètre 3 à la longueur totale 2 est d'environ 1: 8, le diamètre 3 étant  A casing 1 of combat head 1 of a rocket not shown has a length 2 for a diameter 3 of a cylindrical portion 4. The ratio of diameter 3 to total length 2 is about 1: 8, the diameter 3 being

de 100 mm et l'épaisseur 5 de 3 mm.  100 mm and the thickness 5 of 3 mm.

A l'extrémité antérieure d'une section en ogive se trouve une partie d'embouchure 11 épaissie, comportant  At the front end of an ogive section is a thickened mouth portion 11, comprising

un taraudage 12.a tapping 12.

La matière constituant l'enveloppe 1 de la tête consiste en de l'acier de désignation 015, c'est-à-dire d'une  The material constituting the casing 1 of the head consists of steel of designation 015, that is to say of a

teneur en carbone de 0,15%.carbon content of 0.15%.

REVX7IEND I C AT I ONSREVX7IEND I C AT I ONS

1. Enveloppe de tête de combat de projectile à gros calibre ou de fusée, comprenant une section en ogive et une section cylindrique qui lui est reliée, le rapport du diamètre extérieur à la longueur totale étant d'environ 1: 4 à 1: 10, caractérisé en ce que l'enveloppe (1) de la tête est réalisée d'un seul tenant et est constituée par une matière susceptible d'être usinée par fluage sous pression,  1. Large-caliber projectile or rocket combat head shell, comprising an ogival section and a cylindrical section connected thereto, the ratio of outer diameter to total length being approximately 1: 4 to 1: 10 , characterized in that the envelope (1) of the head is made in one piece and is constituted by a material capable of being machined by creep under pressure,

telle que de l'acier au carbone.such as carbon steel.

2. Enveloppe de tête de combat selon la revendication 1, caractérisée en ce qu'elle comporte une partie d'embouchure  2. combat head shell according to claim 1, characterized in that it comprises a mouth portion

(11) épaissie pourvue d'un taraudage (12).  (11) thickened provided with a thread (12).

3. Enveloppe de tête de combat selon la revendica-  3. Combat head shell according to the claim

tion 1, caractérisé en ce que l'épaisseur (5) de la paroi  1, characterized in that the thickness (5) of the wall

est constante jusqu'à la partie d'embouchure (11).  is constant up to the mouth portion (11).

FR8515870A 1984-11-27 1985-10-25 COMBAT HEAD OF A LARGE SIZE PROJECTILE OR A ROCKET Pending FR2573681A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19843443195 DE3443195A1 (en) 1984-11-27 1984-11-27 WARBALL HEAD OF A LARGE-BULLETED BULLET OR A ROCKET

Publications (1)

Publication Number Publication Date
FR2573681A1 true FR2573681A1 (en) 1986-05-30

Family

ID=6251265

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8515870A Pending FR2573681A1 (en) 1984-11-27 1985-10-25 COMBAT HEAD OF A LARGE SIZE PROJECTILE OR A ROCKET

Country Status (4)

Country Link
DE (1) DE3443195A1 (en)
FR (1) FR2573681A1 (en)
GB (1) GB2168133B (en)
IT (2) IT1186197B (en)

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB100128A (en) * 1915-03-02 1916-09-21 Bethlehem Steel Corp An Improved Projectile and Method of Making same.
GB227730A (en) * 1924-07-04 1925-01-22 John Cockerill Soc A projectile for use against submarines
FR815808A (en) * 1936-03-30 1937-07-23 Tubes De Valenciennes Et Denai Welded base shell and its manufacturing process
GB571542A (en) * 1942-10-17 1945-08-29 Platers & Stampers Ltd Improvements in or relating to high explosive projectiles and method of producing the same
GB933114A (en) * 1960-06-29 1963-08-08 Hotchkiss Brandt Improved projectile for a mortar having a non-rifled bore
GB1223931A (en) * 1967-06-09 1971-03-03 Brevets Aero Mecaniques Improvements in or relating to spin-stabilized explosive shell with base detonating fuse
GB1396279A (en) * 1966-01-26 1975-06-04 Cross C S Projectile
US3995550A (en) * 1975-12-03 1976-12-07 The United States Of America As Represented By The Secretary Of The Army Apparatus for stabilizing a liquid filled artillery projectile
GB1510986A (en) * 1974-08-03 1978-05-17 Rheinmetall Gmbh Projectile with an ejectable payload
GB1584044A (en) * 1976-08-24 1981-02-04 Raufoss Ammunisjonsfabrikker Projectile for scattering of a load

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1181043A (en) * 1968-09-21 1970-02-11 Bengt Robert Wilhelm Moldeus Improvements in or relating to Cartridges for Barrage Defence Purposes
DE2654827A1 (en) * 1976-12-03 1978-06-08 Rheinmetall Gmbh HOLLOW LOADING SUB-FLOOR SHOULD BE SHOCKED WITH A CARRIER BULLET
DE3209594A1 (en) * 1982-03-17 1983-09-29 L'Etat Français représenté par le Délégué Général pour l'Armement, 75997 Paris TARGET-BREAKING RIFLE SHEET, IN PARTICULAR TO FIGHT MULTIPLE-PLATE TARGETS

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB100128A (en) * 1915-03-02 1916-09-21 Bethlehem Steel Corp An Improved Projectile and Method of Making same.
GB227730A (en) * 1924-07-04 1925-01-22 John Cockerill Soc A projectile for use against submarines
FR815808A (en) * 1936-03-30 1937-07-23 Tubes De Valenciennes Et Denai Welded base shell and its manufacturing process
GB571542A (en) * 1942-10-17 1945-08-29 Platers & Stampers Ltd Improvements in or relating to high explosive projectiles and method of producing the same
GB933114A (en) * 1960-06-29 1963-08-08 Hotchkiss Brandt Improved projectile for a mortar having a non-rifled bore
GB1396279A (en) * 1966-01-26 1975-06-04 Cross C S Projectile
GB1223931A (en) * 1967-06-09 1971-03-03 Brevets Aero Mecaniques Improvements in or relating to spin-stabilized explosive shell with base detonating fuse
GB1510986A (en) * 1974-08-03 1978-05-17 Rheinmetall Gmbh Projectile with an ejectable payload
US3995550A (en) * 1975-12-03 1976-12-07 The United States Of America As Represented By The Secretary Of The Army Apparatus for stabilizing a liquid filled artillery projectile
GB1584044A (en) * 1976-08-24 1981-02-04 Raufoss Ammunisjonsfabrikker Projectile for scattering of a load

Also Published As

Publication number Publication date
GB2168133A (en) 1986-06-11
GB8529105D0 (en) 1986-01-02
DE3443195A1 (en) 1986-05-28
IT8522871A0 (en) 1985-11-15
IT1186197B (en) 1987-11-18
IT8523847V0 (en) 1985-11-15
GB2168133B (en) 1988-06-22

Similar Documents

Publication Publication Date Title
FR2615937A1 (en) IMPROVEMENTS TO PERFORATING PROJECTILES
FR2764056A1 (en) MOUTH BRAKE FOR WEAPON TUBE
FR2665950A1 (en) AMMUNITION OF A SINGLE PIECE.
CH636191A5 (en) SOCKET AND FIREARMS CARTRIDGE COMPRISING SUCH A SOCKET.
BE900838A (en) THREADED POLAR OPENINGS FOR PRESSURE COMPOSITE CONTAINERS.
EP1475601B1 (en) Subcalibre projectile, rod and sabot constituting such a projectile
FR2573681A1 (en) COMBAT HEAD OF A LARGE SIZE PROJECTILE OR A ROCKET
EP3715776B1 (en) Cartridge comprising fuse cords
EP0048644A1 (en) Vaned projectile of the arrow type
FR2535839A1 (en) BULLET CARTRIDGE FOR RIFLE
KR850000894A (en) ACRO Composite Electrode
FR2721390A1 (en) Anti-curvature attachment for large-calibre artillery piece barrel
WO1992017746A1 (en) Revolver mortar
FR2526153A1 (en) Sub-calibre projectile with propelling ring - comprising outer deformable plastics cylinder and inner metal cone
EP0169585A1 (en) Fragmentation-type shell
FR2820672A1 (en) HOLDER PISTON
FR2699659A1 (en) Breakable join device between front and rear sections of munition
WO1984002182A1 (en) Improvements to projectiles intended to be fired by a fire-arm
FR2671619A1 (en) EXPLOSIVE CHARGE TRIM FORMING PROJECTILE.
FR2692033A1 (en) Projectile unit for a large caliber tube gun.
CH637761A5 (en) ASSEMBLY CONSISTING OF A PROJECTILE AND THE DEVICE FOR LAUNCHING THE PROJECTILE.
FR2574921A2 (en) One-piece projectile device launched by a portable firearm
EP0486077B1 (en) Rifle grenade
BE1002303A3 (en) Improvements to the constrictions for hunting arms
FR2564911A1 (en) Assembly comprising a composite tubular element and a tapped metal end piece for connection.