GB2353087A - Deploying submunitions such as decoys - Google Patents
Deploying submunitions such as decoys Download PDFInfo
- Publication number
- GB2353087A GB2353087A GB0013667A GB0013667A GB2353087A GB 2353087 A GB2353087 A GB 2353087A GB 0013667 A GB0013667 A GB 0013667A GB 0013667 A GB0013667 A GB 0013667A GB 2353087 A GB2353087 A GB 2353087A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ammunition
- interface
- sub
- munitions
- thrower
- 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.)
- Granted
Links
- 238000010304 firing Methods 0.000 claims abstract description 12
- 230000000694 effects Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 230000002123 temporal effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/145—Cartridges, i.e. cases with charge and missile for dispensing gases, vapours, powders, particles or chemically-reactive substances
- F42B5/15—Cartridges, i.e. cases with charge and missile for dispensing gases, vapours, powders, particles or chemically-reactive substances for creating a screening or decoy effect, e.g. using radar chaff or infrared material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C17/00—Fuze-setting apparatus
- F42C17/04—Fuze-setting apparatus for electric fuzes
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
An ammunition or pyrotechnical device for deploying sub-munitions and/or light signals, the firing sequence of which is controlled electronically, wherein the ammunition presents an externally accessible interface, preferably an infrared interface, for external programming. Thanks to such an ammunition it is possible for the first time to modify the firing sequence of sub-munitions under control by a computer even while located inside a thrower tube.
Description
2353087
Description
Ammunition or pyrotechnical device for deploying sub-munitions, and an ammunitions thrower herefor The present invention relates to an ammunition or a pyrotechnical device for deploying sub-m-unitions and/or light signals in accordance with the preamble of claim 1, and an ammunitions thrower herefor in accordance with claim 11.
Modern decoy ammunitions frequently contain a series of submunitions in one cartridge casing.
When a guided missile is identified during its approach, the decoy ammunition is discharged from an ammunitions thrower. The decoy ammunition may, for example, present a defined infrared signature which has the effect of diverting the guided missile from its target.
To this end, the decoy cartridge is generally ignited by means of the thrower system, and in a definedly programmed temporal sequence the single sub-munitions are discharged in order to lead the guided missile further and further from its actual target.
In the prior art it is known for the electronic control of decoy ammunition to ignite the single sub-munitions in accordance with a fixed, predetermined pattern.
Under practical circumstances this rigid setting of the firing sequence of sub-munitions has, however, been found to be not particularly effective as it frequently passes by the requirements of diverting the approaching guided missile as far as possible from its actual target, which may thus constitute a continued hazard, e.g., to vessels of a naval formation or the craft of an aircraft squadron.
Starting out from the above mentioned prior art, it therefore was the object of the present invention to furnish a thrower system as well as an ammunition enabling variation of the sub-munitions firing sequences on short notice.
With respect to an ammunition or a pyrotechnical device, this object is attained through the characterising features of claim 1. With respect to a thrower system, the above object is attained through the characterising features of claim 11.
In accordance with the invention, the ammunition or the pyrotechnical device for deploying sub-munitions and/or light signals, the firing sequence of which is controlled electronically, includes an externally accessible interface for external programming.
Hereby it is possible to quickly adapt to particular environmental conditions such as, e.g., strong winds, and to program the ammunition in such a way that it will present optimum results under wartime conditions.
In accordance with claim 2, a decoy ammunition is preferred which, owing to the possibility of external programming, enables optimum adaptation of the ammunition to particular circumstances, such as, e.g., weather conditions.
In accordance with claim 3, the sub-munitions have different properties, in particular different decoy properties. This has the advantage that depending on the type of ammunition and of the sub-munition contained therein, different guided missiles - or in turn guided missiles employing different target acquisition techniques - may be warded off.
Thus, for example, a decoy ammunition may contain both infrared decoy ammunitions and radar decoy ammunitions.
Moreover it is conceivable that the sub-munitions present different infrared signatures.
In accordance with claim 4, the interface may be a conventional plug type connection, such as, for example, a parallel or serial interface, e. g., of the RS 232 or USP types.
Thanks to a like plug-type connection, stocks of ammunition, such as on a ship, may preliminarily be programmed for different scenarios and may then optionally be re-programmed.
In accordance with claim 6, it is preferred that the interface is a wireless connection, in particular an infrared connection in accordance with claim 6. This opens the possibility of re-programming an ammunition already inserted into the thrower tube of a thrower system inside this very thrower tube by way of the thrower system.
This may, for example, be of particular importance if the trajectory of an approaching enemy guided missile is detected following firing of the first sub-munition from the object to be protected, and an optimum period after which firing of the next and the following sub-munitions is to take place is calculated by the computer system.
With this feedback process it is possible to ensure optimum effect in terms of diverting a guided missile and thereby enhance the safety of the object to be protected, such as of a ship, tank, airplane, or stationary object.
Moreover particularly infrared interfaces are extremely robust and have manifold applications.
Preferably the interface of the ammunition is programmed via a programming device or a computer, in particular a personal computer, wherein the computer may, for example, also access the program memory of the ammunition by way of the thrower system.
It is particularly preferred to program the firing sequence of the submunitions by way of the interface contained on the ammunition in accordance with claim 8. A particularly preferred embodiment of the present invention is given in claim 9, namely, due to the fact that the ammunition may be programmed by way of the interface while still inside a thrower tube shortly prior to being discharged, it becomes possible to calculate the optimum firing sequence for the sub-munitions through feedback analysis of the approaching guided missile.
In particular, in accordance with claim 10 the time intervals for deploying sub-munitions or also light signals are programmed via the interface. Thus, for example, a particular light/disintegration pattern may be programmed in the pyrotechnical range.
The instant defense system presents a particularly advantageous configuration if an ammunitions thrower in accordance with claim 11 and/or 12 is used, which is still capable of programming the ammunition for deploying sub-munition or light signals while the ammunition is already located inside the thrower tube.
Another advantage of the inventive thrower system comprised of ammunition and ammunitions thrower is founded in the fact that not only the firing sequence of the sub-munitions can be optimised, but furthermore only a quantity of sub-munition definitely necessary for warding off an approaching guided missile must be fired.
As the stocks of ammunition in an object to be protected are inherently limited, this circumstance is of particular importance.
In a particularly advantageous manner, the inventive ammunition, in particular cartridge, is combined with a device for simulating (emulating) an empty load status of a thrower for cartridges in accordance with the German patent application entitled, "Vorrichtung zur Nachbildung (Emulation) eines Leerzustandes eines Werfers fOr Patronen sowie Patrone hiermit", by the present applicant and having the file number BU2966 of the same application date, the contents of which are herewith fully incorporated by way of reference.
Claims (12)
1 An ammunition or pyrotechnical device for deploying sub munitions and/or light signals, the firing sequence of which is controlled electronically, characterised in that said ammunition presents an externally accessible interface for external programming.
2. An ammunition according to claim 1, characterised by being a decoy ammunition.
3. An ammunition according to claim 1 or 2, characterised in that said sub-munitions have different properties, in particular different decoy properties.
4. An ammunition according to any one of claims 1 to 3, characterised in that said interface is a plug-type connection.
5. An ammunition according to any one of claims 1 to 3, characterised in that said interface is a wireless connection.
6. An ammunition according to claim 5, characterised in that said interface is an infrared interface.
7. An ammunition according to any one of claims 1 to 6, characterised in that said interface may be programmed through a programming device or a computer, in particular a personal computer.
8. An ammunition according to any one of claims 1 to 7, characterised in that the firing sequence of said sub-munitions may be programmed by way of said interface.
9. An ammunition according to any one of claims 1 to 8, characterised in that it may still be programmed by way of said interface while located inside a thrower tube.
10. An ammunition according to any one of claims 1 to 9, characterised in that the time intervals for deploying said submunitions or light signals may be programmed through said interface.
11. Ammunitions thrower, characterised in that it presents an interface for programming an ammunition according to at least one of claims 1 to 7.
12. The ammunitions thrower according to claim 11, characterised in that said interface is an infrared interface.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1999136587 DE19936587C2 (en) | 1999-08-04 | 1999-08-04 | Ammunition or pyrotechnic device for deploying submunitions |
Publications (3)
Publication Number | Publication Date |
---|---|
GB0013667D0 GB0013667D0 (en) | 2000-07-26 |
GB2353087A true GB2353087A (en) | 2001-02-14 |
GB2353087B GB2353087B (en) | 2004-01-07 |
Family
ID=7917083
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0013667A Expired - Lifetime GB2353087B (en) | 1999-08-04 | 2000-06-05 | Ammunition for deploying sub-munitions |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE19936587C2 (en) |
GB (1) | GB2353087B (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2374134A (en) * | 2001-04-04 | 2002-10-09 | Buck Neue Technologien Gmbh | Method and apparatus for the protection of mobile military facilities |
WO2007087948A1 (en) * | 2006-01-20 | 2007-08-09 | Rheinmetall Waffe Munition Gmbh | System for protection in particular of large flying platforms against infrared and/or radar-guided threats |
US7373886B2 (en) | 2001-05-07 | 2008-05-20 | Saab Ab | Dispenser for discharging countermeasures and method therefore |
WO2009006981A1 (en) | 2007-07-09 | 2009-01-15 | Rheinmetall Waffe Munition Gmbh | Method and launching apparatus for protection of an object against a threat, in particular a missile, as well as munition |
US7600477B2 (en) | 2001-05-07 | 2009-10-13 | Saab Ab | Method for discharging countermeasure means, rocket launcher, and dispenser arrangement |
US7886646B2 (en) | 2003-10-02 | 2011-02-15 | Rheinmetall Waffe Munition Gmbh | Method and apparatus for protecting ships against terminal phase-guided missiles |
WO2011101692A1 (en) * | 2010-02-17 | 2011-08-25 | Wallop Defence Systems Limited | Air countermeasure cartridge |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2138456A (en) * | 1983-03-25 | 1984-10-24 | Textima Veb K | A process and an apparatus for fibre fleece production |
DE3427164A1 (en) * | 1984-07-24 | 1986-01-30 | Dynamit Nobel Ag, 5210 Troisdorf | Missile with submunition |
US4586439A (en) * | 1983-05-03 | 1986-05-06 | U.S. Philips Corporation | Cartridge for launching decoys |
EP0233833A1 (en) * | 1986-01-31 | 1987-08-26 | Loral Corporation | Spin dispensing method and apparatus |
EP0282394A1 (en) * | 1987-03-04 | 1988-09-14 | R. ALKAN & Cie. | Selective bullet-shooting apparatus and method for an aircraft or other machines |
EP0536101A1 (en) * | 1991-10-02 | 1993-04-07 | CelsiusTech Electronics AB | Release unit, and release system comprising at least one such release unit |
WO1993014365A1 (en) * | 1992-01-07 | 1993-07-22 | The Walt Disney Company | Precision fireworks display system having a decreased environmental impact |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3636055C1 (en) * | 1986-10-23 | 1989-12-21 | Messerschmitt Boelkow Blohm | Submunition release device |
DE3800407C1 (en) * | 1988-01-09 | 1989-03-23 | Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De | Different distribution of submunitions |
-
1999
- 1999-08-04 DE DE1999136587 patent/DE19936587C2/en not_active Expired - Lifetime
-
2000
- 2000-06-05 GB GB0013667A patent/GB2353087B/en not_active Expired - Lifetime
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2138456A (en) * | 1983-03-25 | 1984-10-24 | Textima Veb K | A process and an apparatus for fibre fleece production |
US4586439A (en) * | 1983-05-03 | 1986-05-06 | U.S. Philips Corporation | Cartridge for launching decoys |
DE3427164A1 (en) * | 1984-07-24 | 1986-01-30 | Dynamit Nobel Ag, 5210 Troisdorf | Missile with submunition |
EP0233833A1 (en) * | 1986-01-31 | 1987-08-26 | Loral Corporation | Spin dispensing method and apparatus |
EP0282394A1 (en) * | 1987-03-04 | 1988-09-14 | R. ALKAN & Cie. | Selective bullet-shooting apparatus and method for an aircraft or other machines |
EP0536101A1 (en) * | 1991-10-02 | 1993-04-07 | CelsiusTech Electronics AB | Release unit, and release system comprising at least one such release unit |
WO1993014365A1 (en) * | 1992-01-07 | 1993-07-22 | The Walt Disney Company | Precision fireworks display system having a decreased environmental impact |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2374134A (en) * | 2001-04-04 | 2002-10-09 | Buck Neue Technologien Gmbh | Method and apparatus for the protection of mobile military facilities |
GB2374134B (en) * | 2001-04-04 | 2004-09-15 | Buck Neue Technologien Gmbh | Method and apparatus for the protection of mobile military facilities |
US7373886B2 (en) | 2001-05-07 | 2008-05-20 | Saab Ab | Dispenser for discharging countermeasures and method therefore |
US7600477B2 (en) | 2001-05-07 | 2009-10-13 | Saab Ab | Method for discharging countermeasure means, rocket launcher, and dispenser arrangement |
US7886646B2 (en) | 2003-10-02 | 2011-02-15 | Rheinmetall Waffe Munition Gmbh | Method and apparatus for protecting ships against terminal phase-guided missiles |
WO2007087948A1 (en) * | 2006-01-20 | 2007-08-09 | Rheinmetall Waffe Munition Gmbh | System for protection in particular of large flying platforms against infrared and/or radar-guided threats |
WO2009006981A1 (en) | 2007-07-09 | 2009-01-15 | Rheinmetall Waffe Munition Gmbh | Method and launching apparatus for protection of an object against a threat, in particular a missile, as well as munition |
WO2011101692A1 (en) * | 2010-02-17 | 2011-08-25 | Wallop Defence Systems Limited | Air countermeasure cartridge |
Also Published As
Publication number | Publication date |
---|---|
DE19936587C2 (en) | 2003-08-21 |
DE19936587A1 (en) | 2001-02-22 |
GB0013667D0 (en) | 2000-07-26 |
GB2353087B (en) | 2004-01-07 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN1165740C (en) | Decoy | |
US20020149510A1 (en) | Method and apparatus for the protection of mobile military facilities | |
US20080006171A1 (en) | XM-5866 Stingball flashbang grenade | |
EP2549221B1 (en) | Ammunition | |
US20100288111A1 (en) | Method and launching apparatus for protection of an object against a threat, in particular a missile, as well as munition | |
DE102007007404A1 (en) | Method and device for remote release of a projectile | |
GB2353087A (en) | Deploying submunitions such as decoys | |
DE102009016147A1 (en) | Demountable projectile for use in weapon barrel of weapon system, is demounted into two projectile parts after firing target location, where projectile parts are connected with each other by multiple connecting elements | |
DE102005043078A1 (en) | Sensor fused munition | |
DE3844974C2 (en) | Practice bomblet | |
US7481145B1 (en) | Cruise munitions detonator projectile | |
WO2009046799A1 (en) | Explosive projectile for artillery or mortar | |
US10598471B2 (en) | Self-consuming projectile | |
GB2410786A (en) | Method and apparatus for the protection of battlefield vehicles | |
EP3887750B1 (en) | Practice ammunition and training system using the practice ammunition | |
GB2192258A (en) | Non-lethal ammunition | |
EP0791800B1 (en) | Anti-missile missiles | |
US5824939A (en) | System and method for deceiving enemy forces in battlefield | |
RU2146352C1 (en) | Antirocket rocket | |
DE102013010357A1 (en) | Projectile with effect or signal effect | |
KR101899657B1 (en) | Apparatus for controlling naval artillery and method thereof | |
EP3546881B1 (en) | Projectile with base igniter and marking charge | |
RU194887U1 (en) | Combat vehicle fire control system | |
EP1087202B1 (en) | Armour perforating ammunition | |
DE3004317A1 (en) | Firing system for anti-helicopter projectiles - takes target movement into account whilst missile is in flight, using flight path computer |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PE20 | Patent expired after termination of 20 years |
Expiry date: 20200604 |