CA1303905C - High-explosive device for the engagement of armoured targets - Google Patents
High-explosive device for the engagement of armoured targetsInfo
- Publication number
- CA1303905C CA1303905C CA000539902A CA539902A CA1303905C CA 1303905 C CA1303905 C CA 1303905C CA 000539902 A CA000539902 A CA 000539902A CA 539902 A CA539902 A CA 539902A CA 1303905 C CA1303905 C CA 1303905C
- Authority
- CA
- Canada
- Prior art keywords
- charge
- insert
- munition
- target
- channel
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B1/00—Explosive charges characterised by form or shape but not dependent on shape of container
- F42B1/02—Shaped or hollow charges
- F42B1/032—Shaped or hollow charges characterised by the material of the liner
-
- 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
- F42B12/16—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 in combination with an additional projectile or charge, acting successively on the target
- F42B12/18—Hollow charges in tandem arrangement
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
- Optical Radar Systems And Details Thereof (AREA)
- Valve Device For Special Equipments (AREA)
- Valve-Gear Or Valve Arrangements (AREA)
- Agricultural Chemicals And Associated Chemicals (AREA)
- Chemical And Physical Treatments For Wood And The Like (AREA)
- Fire-Extinguishing Compositions (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
ABSTRACT
The high-explosive device has a rear hollow charge 12 with a liner 14 and, axially separated from and ahead of this, a charge with a flat insert 20 that forms a projectile. On approaching a target that is to be engaged, the charges 18 and 12 are initiated in sequence, so that the projectile formed from the insert 20 is effective at the target ahead of the jet that is formed by the liner 14.
The high-explosive device has a rear hollow charge 12 with a liner 14 and, axially separated from and ahead of this, a charge with a flat insert 20 that forms a projectile. On approaching a target that is to be engaged, the charges 18 and 12 are initiated in sequence, so that the projectile formed from the insert 20 is effective at the target ahead of the jet that is formed by the liner 14.
Description
~3~
1 26130-~7 The present invention relates to a hiqh-explosive munition device for the engagementr in particular the active engagement, of armoured targets.
DE-OS 34 16 787 discloses such a high-explosive devi~e incorporating ~wo charges, arranged in tandem and inltiated by means provided for this purpose, kinetic energy being generated at the target from the first charge, in order to render harmless an interference system at the target, so that subsequently a hollow-charge jet from the second charge can be unrestrictedly effective at the target. The two charges are essentially of the same diameter, and each of them is arranged in its own housing with stabilizlng fins. After initiation of a separation charge, each forms an indepeadent projectile.
This known arrangement is not only complicated and extremely costly from the point of view of space and production;
it also entails a large amount of dead weight that has no effect at the target. These disadvantages come into play in operations of all kinds such that it becomes a matter of urgency to create a device of this type, which includes very little dead welght and takes up only a small amount of space.
The present invention provides an active munition element for combatting a target provided with a jamming devlce, the munition element comprising: a shaped front chaxge element includlng a front insert and a front charge behlnd said front insert; a shaped rear charge element including a rear inser~
mounted behind said front charge and a rear charge behind said rear insert; means, including a proximity fuze for igniting said front charge, connected for actuating said front charge at a given .
~3~3~S
1 26130-~7 The present invention relates to a hiqh-explosive munition device for the engagementr in particular the active engagement, of armoured targets.
DE-OS 34 16 787 discloses such a high-explosive devi~e incorporating ~wo charges, arranged in tandem and inltiated by means provided for this purpose, kinetic energy being generated at the target from the first charge, in order to render harmless an interference system at the target, so that subsequently a hollow-charge jet from the second charge can be unrestrictedly effective at the target. The two charges are essentially of the same diameter, and each of them is arranged in its own housing with stabilizlng fins. After initiation of a separation charge, each forms an indepeadent projectile.
This known arrangement is not only complicated and extremely costly from the point of view of space and production;
it also entails a large amount of dead weight that has no effect at the target. These disadvantages come into play in operations of all kinds such that it becomes a matter of urgency to create a device of this type, which includes very little dead welght and takes up only a small amount of space.
The present invention provides an active munition element for combatting a target provided with a jamming devlce, the munition element comprising: a shaped front chaxge element includlng a front insert and a front charge behlnd said front insert; a shaped rear charge element including a rear inser~
mounted behind said front charge and a rear charge behind said rear insert; means, including a proximity fuze for igniting said front charge, connected for actuating said front charge at a given .
~3~3~S
distance ahead of the target in order to develop kinetic energy in the taryet so as to neutralize the jamming device; means for actuating said rear charge after actuation of said front charge with a given time delay so as to be effective against the target without interference from ~ha jamming device; and a tube means deflning a narrow longitudinal channel having a smaller diameter than, and coaxial with, said rear charge element, said channel extending forwardly from said rear insert so as to direct said rear insert therethrough upon actuation of said rear charge, said channel having a front end region housing said front charge.
The invention wlll further be descrlbed in yreater detail below, and by way of example only, on the bas.ls of the drawings appended hereto, wherein:-Figure 1 is a simplified illustration of the principles of the high-explosive munition element according ~o the present invention, shown in longitudinal sertion;
Figure 2 shows a warhead that can be ejected from a payload projectile and that can be guided, incorporating the high-explosive device of ~igure 1;
Figure 3 is a prospective view of an aimable antitank missile with the hi~h-explosive device of Figure 1;
Figure 4 shows a fin-stabilized full-calibre antitank projectile.
In Figures 2r 3, and 4, for purposes of greater clari~y, detailed representation of the structure shown in Fiyure 1 has been omitted.
As can be seen from Figure 1, a munition element or projectile 10 has a casing 11 that is rationally symmetrical about .
, - .
:,~ : - . .
- .
' ~ :
3i~
The invention wlll further be descrlbed in yreater detail below, and by way of example only, on the bas.ls of the drawings appended hereto, wherein:-Figure 1 is a simplified illustration of the principles of the high-explosive munition element according ~o the present invention, shown in longitudinal sertion;
Figure 2 shows a warhead that can be ejected from a payload projectile and that can be guided, incorporating the high-explosive device of ~igure 1;
Figure 3 is a prospective view of an aimable antitank missile with the hi~h-explosive device of Figure 1;
Figure 4 shows a fin-stabilized full-calibre antitank projectile.
In Figures 2r 3, and 4, for purposes of greater clari~y, detailed representation of the structure shown in Fiyure 1 has been omitted.
As can be seen from Figure 1, a munition element or projectile 10 has a casing 11 that is rationally symmetrical about .
, - .
:,~ : - . .
- .
' ~ :
3i~
the longitudinal axis A, and contains a charge 12. A connector piece 13 serves to accommodate the systems 22 for supplying power to the control electronics 24. A tube 15 defines a channel 16, coaxial with A, for a shaped-charge jet that is to be formed from a liner or insert 14 once the charge 12 has been initiated. In the front area of the channel 16 the tube 15 serves to accommodate a charge 18 with a casing 19 and a flat insert 20 that forms a projectile.
The munition element or projectile 10 is particularly well-suited for the engagement, in particular the active engagement, of armoured targets. A proximity ~uze, not shown hereln and known in and of itself, sends a signal to tbe control electronics 24 when at a set distance from the target. A first control signal to initiate the forward charge 18 is formed from this signal, and the flat insert projectile 20 precedes the main projectile to the target. At the target, the impact of this first projectile 20 causes the interference system or jamming means to be activated and thus neutralized for the hollow-charge jet that i5 formed from the insert 14 of the rear charge 12 that is initiated by a second control signal. The "interference suppression" effect at the target is thus achieved by means that take up very li~tle space, with very little dead-weight, and without the complicated separation charge that renclars the projectile vulnerable to jamming, as is known from the cited publicat1On.
The flat insert 20 of the front charge lB consists preferably of a material having an averaga density of between approximately 16 and approximately 19 g~am3. This means ~ha~
,, .
3a 26130-47 because of the correspondingly great kinetic energy effect of the projectile formed by the inser~ 20 by explosive force, the jammin~
~eans or interference system at the target will ~ith a high degree of probability, -- . .
.
,, ~ ' :L3~3)3~3~i be rendered innocuous so that the hollow charge jet from the insert 14 can be totally effective at the target. It is also possible to achieve a more effective standoff because of this. 3ecause of the comparitive smallness of the insert 20 the advantage arises that the price of the insert material does not play a very great role, so that, for example, there is no real cost barrier to the use of tantalum.
On examining Figures 2, 3, and 4 in conjunction with the foregoing description it can be seen how versatile the pro-jectile 10 according to the present invention is.
As is shown in Figure 2, the high-explosive device 10 is incorporated in a warhead 40 that can be ejected from a carrier pro~ectile as a controllable submunition unit. In this connection, reference is made to a brochure issued by Allied Bendix Aerospace and the applicant Rheinmetall GmbH that has been published since October 1985. The connector 13' extends as far as a target-seeking head 52, known in and of itself, and serves to accommodate the electronics 44 and a control unit 46 with gas generators 48 and control nozzles 50; the above systems and devices are grouped behind the target-seeking head 52, around the tube 15 with the channel 16 so as to take up very little space. Stabilizing fins 42 can be pivoted in known familiar manner from a space~saving transportation position into the operating position shown in the drawing. The direction of flight of the warhead 40 with the high-explosive device 10 is indicated by the arrow F.
As is shown in Figure 3, the high-explosive device 10, :, ~
.
`` 13~.~3~
The munition element or projectile 10 is particularly well-suited for the engagement, in particular the active engagement, of armoured targets. A proximity ~uze, not shown hereln and known in and of itself, sends a signal to tbe control electronics 24 when at a set distance from the target. A first control signal to initiate the forward charge 18 is formed from this signal, and the flat insert projectile 20 precedes the main projectile to the target. At the target, the impact of this first projectile 20 causes the interference system or jamming means to be activated and thus neutralized for the hollow-charge jet that i5 formed from the insert 14 of the rear charge 12 that is initiated by a second control signal. The "interference suppression" effect at the target is thus achieved by means that take up very li~tle space, with very little dead-weight, and without the complicated separation charge that renclars the projectile vulnerable to jamming, as is known from the cited publicat1On.
The flat insert 20 of the front charge lB consists preferably of a material having an averaga density of between approximately 16 and approximately 19 g~am3. This means ~ha~
,, .
3a 26130-47 because of the correspondingly great kinetic energy effect of the projectile formed by the inser~ 20 by explosive force, the jammin~
~eans or interference system at the target will ~ith a high degree of probability, -- . .
.
,, ~ ' :L3~3)3~3~i be rendered innocuous so that the hollow charge jet from the insert 14 can be totally effective at the target. It is also possible to achieve a more effective standoff because of this. 3ecause of the comparitive smallness of the insert 20 the advantage arises that the price of the insert material does not play a very great role, so that, for example, there is no real cost barrier to the use of tantalum.
On examining Figures 2, 3, and 4 in conjunction with the foregoing description it can be seen how versatile the pro-jectile 10 according to the present invention is.
As is shown in Figure 2, the high-explosive device 10 is incorporated in a warhead 40 that can be ejected from a carrier pro~ectile as a controllable submunition unit. In this connection, reference is made to a brochure issued by Allied Bendix Aerospace and the applicant Rheinmetall GmbH that has been published since October 1985. The connector 13' extends as far as a target-seeking head 52, known in and of itself, and serves to accommodate the electronics 44 and a control unit 46 with gas generators 48 and control nozzles 50; the above systems and devices are grouped behind the target-seeking head 52, around the tube 15 with the channel 16 so as to take up very little space. Stabilizing fins 42 can be pivoted in known familiar manner from a space~saving transportation position into the operating position shown in the drawing. The direction of flight of the warhead 40 with the high-explosive device 10 is indicated by the arrow F.
As is shown in Figure 3, the high-explosive device 10, :, ~
.
`` 13~.~3~
- 5 - 26].3~-47 slightly modified (reference is made to -the configuration of the liner 64), has been integrated into an aimable antitank projectile 60. This comprises a launcher tube 62 on a tripod m~unt 74. The central longitudinal axis (not shown herein) of a known sighting system 66, which incorporates the necessary control electronics) is parallel to the longitudinal axis A. A rocket motor 70 can be initiated through the firing system 68. The launcher tube 68 is so adjusted by means of the mount 74 that its longitudinal axis is trained onto an area in which armoured targets that are to be engaged are anticipated. Once the sighting system 66 has identified such a target, a signal initiates the firing system and this in turn ignites the rocket motor 70. The high-explosive device 10 leaves the tube 62 in the direction indicated by the arrow F after the cover 76 has been blown off, and the stabilizing fins 72 are deployed from their retracted or stowed position as shown in the drawing to their operating position. The operating sequence is described in conjunction with Figure 1.
Figure 4 shows an antitank projectile 80 in the form of a known munition for a cannon. With the exception of conical liner 84 for the rear charge 12, details of the integrated high-explosive device have been omitted. The tube 15 is formed as a standoff tube 82 which, at the front, has a known and thus not further detailed or described proximity fuze a6. A known, fixed stabilizing tail assembly 90 is arranged on the tail shaft 88.
.; , .: ' :
: , .
': :
Figure 4 shows an antitank projectile 80 in the form of a known munition for a cannon. With the exception of conical liner 84 for the rear charge 12, details of the integrated high-explosive device have been omitted. The tube 15 is formed as a standoff tube 82 which, at the front, has a known and thus not further detailed or described proximity fuze a6. A known, fixed stabilizing tail assembly 90 is arranged on the tail shaft 88.
.; , .: ' :
: , .
': :
Claims (8)
1. An active munition element for combatting a target provided with a jamming device, the munition element comprising:
a shaped front charge element including a front insert and a front charge behind said front insert, a shaped rear charge element including a rear insert mounted behind said front charge and a rear charge behind said rear insert;
means, including a proximity fuze for igniting said front charge, connected for actuating said front charge at a given distance ahead of the target in order to develop kinetic energy in the target so as to neutralize the jamming device;
means for actuating said rear charge after actuation of said front charge with a given time delay so as to be effective against the target without interference from the jamming device; and a tube means defining a narrow longitudinal channel having a smaller diameter than, and coaxial with, said rear charge element, said channel extending forwardly from said rear insert so as to direct said rear insert therethrough upon actuation of said rear charge, said channel having a front end region housing said front charge.
a shaped front charge element including a front insert and a front charge behind said front insert, a shaped rear charge element including a rear insert mounted behind said front charge and a rear charge behind said rear insert;
means, including a proximity fuze for igniting said front charge, connected for actuating said front charge at a given distance ahead of the target in order to develop kinetic energy in the target so as to neutralize the jamming device;
means for actuating said rear charge after actuation of said front charge with a given time delay so as to be effective against the target without interference from the jamming device; and a tube means defining a narrow longitudinal channel having a smaller diameter than, and coaxial with, said rear charge element, said channel extending forwardly from said rear insert so as to direct said rear insert therethrough upon actuation of said rear charge, said channel having a front end region housing said front charge.
2. A munition element as defined in claim 1 in combination with, and mounted in, a warhead having a target seeking device.
3. A munition element as defined in claim 1 in combination with, and loaded in, a directional antitank mine.
4. A munition element as defined in claim 1 further comprising an energy source for supplying energy for actuating said charges, and wherein said energy source and said means for actuating each said charge are disposed around the circumference of said tube means.
5. A munition element as defined in claim 1 in combination with a fin stabilized antitank projectile having a subcaliber stand-off tube containing said means defining a channel.
6. A munition element as defined in claim 1 wherein said front insert comprises a projectile forming element in the form of a body of material having an average density of between about 16 and 19 g/cm3.
7. A munition element as in claim 1, wherein said front element is flat and housed in said front end region of said channel.
8. A munition element as in claim 1, wherein said proximity fuze is disposed in front of said front insert.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DEP3619791.2-15 | 1986-06-18 | ||
| DE19863619791 DE3619791A1 (en) | 1986-06-18 | 1986-06-18 | ACTIVITIES TO COMBAT, PARTICULARLY ACTIVE, ARMORED TARGETS |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA1303905C true CA1303905C (en) | 1992-06-23 |
Family
ID=6302869
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA000539902A Expired - Lifetime CA1303905C (en) | 1986-06-18 | 1987-06-17 | High-explosive device for the engagement of armoured targets |
Country Status (9)
| Country | Link |
|---|---|
| EP (1) | EP0249678B2 (en) |
| JP (1) | JPS62299700A (en) |
| AT (1) | ATE55831T1 (en) |
| CA (1) | CA1303905C (en) |
| DE (2) | DE3619791A1 (en) |
| ES (1) | ES2016939B3 (en) |
| IL (1) | IL82794A0 (en) |
| NO (1) | NO871542L (en) |
| ZA (1) | ZA874366B (en) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3924087C1 (en) * | 1989-07-20 | 1997-05-28 | Rheinmetall Ind Ag | Tandem battle head for combating active targets with two parts |
| DE3926711C2 (en) * | 1989-08-12 | 1995-12-07 | Rheinmetall Ind Gmbh | Storey with interior |
| DE3934850C1 (en) * | 1989-10-19 | 2000-09-28 | Daimlerchrysler Aerospace Ag | Tandem munitions head e.g. for long-range missile, has deformable structure for protecting main explosive charge upon detonation of initial explosive charge |
| DE4012163A1 (en) * | 1990-04-14 | 1991-10-17 | Heraeus Gmbh W C | METHOD FOR PRODUCING TANTALE HOLLOW BODIES |
| DE4117871C1 (en) * | 1991-05-31 | 1999-08-19 | Diehl Stiftung & Co | Hollow charge warhead used as a 'tandem' warhead for triggering reactive armor and then forming a hollow charge spike |
| DE19617221C2 (en) * | 1996-04-30 | 1999-07-01 | Diehl Stiftung & Co | Steerable projectile that can be used as a mortar |
| RU193124U1 (en) * | 2019-07-12 | 2019-10-15 | Федеральное государственное бюджетное военное образовательное учреждение высшего образования "Черноморское высшее военно-морское ордена Красной Звезды училище имени П.С. Нахимова" Министерства обороны Российской Федерации | Universal cumulative mine |
| DE102020001784A1 (en) * | 2020-03-17 | 2021-09-23 | Diehl Defence Gmbh & Co. Kg | Projectile, device arrangement and method |
| DE102020113411A1 (en) | 2020-05-18 | 2021-11-18 | Rheinmetall Waffe Munition Gmbh | Device of a defense technology effector |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR999974A (en) * | 1946-02-11 | 1952-02-06 | Soc Tech De Rech Ind | Improvements to shaped charge machines |
| FR2310547A1 (en) * | 1975-05-06 | 1976-12-03 | Realisa Et Applic Tech Et | Missile with secondary charge ahead of main charge - has small charge on nose cone positioned not to disturb main explosion |
| DE2829002C2 (en) * | 1978-07-01 | 1985-04-04 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Warhead |
| SE449528B (en) * | 1983-05-13 | 1987-05-04 | Bofors Ab | ARM BREAKING PROJECT |
| DE3336516C2 (en) * | 1983-10-07 | 1985-09-05 | Bayerische Metallwerke GmbH, 7530 Pforzheim | Lining and allocation for hollow, flat and projectile cargoes |
| FR2581749B1 (en) * | 1985-05-10 | 1987-10-02 | France Etat Armement | ANTICHAR PROJECTILE |
| DE3601051C1 (en) * | 1986-01-16 | 1987-06-11 | Messerschmitt Boelkow Blohm | Warhead |
-
1986
- 1986-06-18 DE DE19863619791 patent/DE3619791A1/en active Granted
-
1987
- 1987-02-24 EP EP87102607A patent/EP0249678B2/en not_active Expired - Lifetime
- 1987-02-24 DE DE8787102607T patent/DE3764406D1/en not_active Expired - Fee Related
- 1987-02-24 AT AT87102607T patent/ATE55831T1/en not_active IP Right Cessation
- 1987-02-24 ES ES87102607T patent/ES2016939B3/en not_active Expired - Lifetime
- 1987-04-13 NO NO871542A patent/NO871542L/en unknown
- 1987-04-27 JP JP62102120A patent/JPS62299700A/en active Pending
- 1987-06-08 IL IL82794A patent/IL82794A0/en not_active IP Right Cessation
- 1987-06-17 ZA ZA874366A patent/ZA874366B/en unknown
- 1987-06-17 CA CA000539902A patent/CA1303905C/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| NO871542L (en) | 1987-12-21 |
| ES2016939B3 (en) | 1990-12-16 |
| EP0249678B1 (en) | 1990-08-22 |
| IL82794A0 (en) | 1987-12-20 |
| ZA874366B (en) | 1987-12-18 |
| DE3764406D1 (en) | 1990-09-27 |
| DE3619791A1 (en) | 1988-01-14 |
| EP0249678A2 (en) | 1987-12-23 |
| EP0249678B2 (en) | 1993-08-18 |
| NO871542D0 (en) | 1987-04-13 |
| JPS62299700A (en) | 1987-12-26 |
| EP0249678A3 (en) | 1988-02-17 |
| ATE55831T1 (en) | 1990-09-15 |
| DE3619791C2 (en) | 1988-04-14 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MKLA | Lapsed |