CA2693006A1 - Method and launching apparatus for protection of an object against a threat, in particular a missile, as well as munition - Google Patents
Method and launching apparatus for protection of an object against a threat, in particular a missile, as well as munition Download PDFInfo
- Publication number
- CA2693006A1 CA2693006A1 CA 2693006 CA2693006A CA2693006A1 CA 2693006 A1 CA2693006 A1 CA 2693006A1 CA 2693006 CA2693006 CA 2693006 CA 2693006 A CA2693006 A CA 2693006A CA 2693006 A1 CA2693006 A1 CA 2693006A1
- Authority
- CA
- Canada
- Prior art keywords
- munitions
- sub
- munition
- light flashes
- threat
- 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.)
- Abandoned
Links
- 238000000034 method Methods 0.000 title claims description 8
- 238000001228 spectrum Methods 0.000 claims abstract description 3
- 230000000977 initiatory effect Effects 0.000 abstract description 4
- 230000002452 interceptive effect Effects 0.000 abstract 1
- 239000000779 smoke Substances 0.000 description 10
- 230000005855 radiation Effects 0.000 description 5
- 235000015842 Hesperis Nutrition 0.000 description 4
- 235000012633 Iberis amara Nutrition 0.000 description 4
- 238000009434 installation Methods 0.000 description 4
- 230000010354 integration Effects 0.000 description 3
- 238000010304 firing Methods 0.000 description 2
- 230000007794 irritation Effects 0.000 description 2
- 230000003287 optical effect Effects 0.000 description 2
- SESFRYSPDFLNCH-UHFFFAOYSA-N benzyl benzoate Chemical compound C=1C=CC=CC=1C(=O)OCC1=CC=CC=C1 SESFRYSPDFLNCH-UHFFFAOYSA-N 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000001151 other effect Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 230000003595 spectral effect Effects 0.000 description 1
- 230000000007 visual 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
- F42B5/03—Cartridges, i.e. cases with charge and missile containing more than one missile
- F42B5/035—Cartridges, i.e. cases with charge and missile containing more than one missile the cartridge or barrel assembly having a plurality of axially stacked projectiles each having a separate propellant charge
-
- 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
Abstract
It is proposed that the functions of camouflage and jamming be absolutely separated. This allows the use of a small-caliber munition (4) which exclusively deploys jammers (6). These jammers (6) or munitions (4) are preferably fired vertically upwards or laterally from the vehicle (object 9) to be protected. For this purpose, the launch barrels (2) are fitted and aligned vertically on the vehicle or the object (9) to be protected. An adequate light flash (8) is produced in the relevant. spectrum by initiation of a pyrotechnic charge, with the initiation being clocked in time and being arranged offset in height, and with the light flash (8) interfering with the aiming mechanism of the approaching warhead. Alternatively, different heights of the break-up flashes can be generated above and/or to the side of the object (9) by a plurality of munitions (4).
Description
Rheinmetall Waffe Munitioli, II euenburg W.BU.0322.WO/DIE June 13, 2008 DESCRIPTION
Method and launching apparatus for protection of an object against a threat, in particular a missile, as well as munition So-called jamming (interference sources) is used, for example, to divert anti-tank guided missiles by means of deployed jammers. Signatures are produced which correspond to the motor of the enemy rockets. The motor is continuously measured in order to control the rockets from the launching apparatus, and the deviation from the expected flight path is carried out by correction of the rockets. This guidance mechanism is influenced by the additional signatures. The rockets are deflected from the flight path.
Jamming can be carried out optically or pyrotechnically. One optical variant is the generation of light flashes by means of a stroboscopic lamp which is fitted in a stationary position on the vehicle. One pyrotechnic variant is pyrotechnic burning in the relevant spectral band by means of a pyrotechnic flare, similar to a Bengal flare.
When pyrotechnic solutions are present in the munitiorl, the jamming is produced by the same munition that is also used to produce the visual blockade (smoke). Light flashes are generated by means of an appropriate break-up charge, integrated in the smoke muriition (DE 38 35 887 C2; DE 28 42 797 C2; DE 10 2005 020 159 A1).
DE 10 2005 054 275 Al describes a self-defence installation for combat vehicles or other objects to be protected. The launch system of the self-defence insta1lation is in this case fitted primarily with a W.BU.0322.WO/DIE - -pyrotechnic munition, in which irritation bodies are included which, immediately after release, produce a powerful light flash and/or smoke. A smoke munition is added to the irritation bodies, for this purpose.
~
J
EP 0 512 202 A2 discloses a method for protection of objects which emit IR radiation, in which, after the missile has been located, a large-area pyrotechnic jamming radiation cloud is produced between the missile and the objet, which cloud first of all briefly emits powerful infrared radiation, which itself interferes with the lock-on and tracking electronics of the homing head. This jamming radiation cloud then emits weak infrared radiation for a comparatively long time. Only after this are a plurality of spoof target clouds created, which deflect the missile step-by-step away from the object to be protected.
The disadvantages of the optical solutions are the high level of technical complexity, the heavy weight and the long firing chain before they become effective.
In the case of pyrotechnic solutions, it has been found that, because of the relatively large munition caliber, it is possible to store and to carry in the vehicle only ammunition for a few missions. Furthermore, the munition is heavy. Furthermore, the ammunition consumption is high because of the normal false-alarm rate.
Conventionally, the munition is fired in the threat direction. This generally depends on alignment of the munition launching installation (DE 10 2005 020 177 A1), which can result in a time delay. A plurality of installatiorls are often necessary in order to allow all threat directions to be covered at the same time (DE 10 2005 054 275 Al).
Vu . i~u . 0~__~ . WG / DT F - ~
Known munition launch installations frequently require a large amount of space and are often difficult to integrate, in particular in vehicles.
A further disadvantage is the muni_tiori itself. 'The functions of jamming and camouflage, for example by means of smoke, are in gerieral always deployed together by this munition. However, smoke iri particular is riot always desirable since it carl impede one's own view.
The invention is based on the object of improved jamming associated with an improved integration capability, by saving weight in the launch installation.
The object is achieved by the features of patent claim 1, patent claim 4 and patent claim 6.
Advantageous embodiments are specified in the dependent claims.
The invention is based on the idea of absolute separation of the functions of camouflage and jamming.
This makes it possible to use a small-caliber munition which deploys exclusively jammers. These jammers or munitions are preferably fired vertically in height and/or laterally by the vehicle (object) to be protected. For this purpose, the launch barrels are fitted and aligned vertically on the vehicle or the object to be protected. Arl adequate light flash is produced in the relevant spectrum by initiation of a pyrotechnic charge, which irlitiat.ion is clocked in time and is arranged offset in height, and the light flash irlterferes with the aiming mechanism of the approaching warhead. Alternatively, different heights of the break-up flashes above and/or to the side of the object can be generated by a plurality of munitions.
W.BU.0322.W0/DIE - 4 -This measure for deployment of the jammers is deployed separately from other effects, such as smoke. The smoke munition, which can be fired separately, then does riot itself need to carry out jamming. This allows a plurality of smoke bodies to be included in the actual smoke munition.
Launching is carried out electrically or mechanically, initiated by a small, compact launching apparatus, for example from magazines. The sub-clocking for initiation of the individual light flashes is controlled by electronics. These electronics are preferably a component of the launching apparatus.
The advantages which result from this are a small launch design, with no aiming elements being required, and lower weight associated with this. Because of the lack of aiming elements, simple integration and a simple technical implementation are possible.
The invention will be explained in more detail using one exemplary embodiment and with reference to the drawing, iri which:
Figure 1 shows a launcher with a munition, Figure 2 shows the munition from Figure 1, and Figure 3 shows an integration optiori on/to a vehicle.
Figure 1 shows a compact launching apparatus or a launcher 1_ in a transparent form, preferably with a plurality of launch barrels 2 which are aligned upward parallel and form a magazine 3. One munition 4 is located in each of these launch barrels 2.
Figure 2 shows the design of the munitions 4. The munition 4 comprises a casing 5 from which one or more W.BU.0322.W0/DIE - 5 -sub-munitioris 6(jammers) are fired. Alternatively, the sub-munitions 6 (jammers) can be fired directly from the magazine 3, without a casing. The munition 4 or sub-munitions 6 has/have a comparatively small caliber for vehicle protectiorl muriitions, for example 40 mm (medium caliber).
The munitions 4 or the sub-munitions 6 have interfaces to the launching apparatus 1, via which they are 10 initiated electrically or mechanically. The sub-clocking for initiatiori of the individual light flashes 8 is controlled by electronics 7. These electronics are preferably a component of the launching apparatus 1. In order to initiate the light flash or break-up flash 8, a plurality of sub-munitions 6 and/or a plurality of munitions 4 can be initiated, clocked in time, successively.
The break-up flashes 8 of the jammers 6 are generated spatially above the vehicle 9 (Figure 3) . The break-up height is preferably in the range from about 3 to 15 m above the vehicle 9. In this case, the height rises within the individual light flashes 8. Firing is preferably carried out from the vehicle 9 vertically upward. A lateral break-up can thus be set, with the break-up taking place with decreasing height.
Figure 3 shows an example of an arrangement of a launching apparatus 1 on a vehicle 9. The break-up flashes 8 are generated at heights of, for example, 4 m, 8 m, or 12 rn above the vehicle 9.
Method and launching apparatus for protection of an object against a threat, in particular a missile, as well as munition So-called jamming (interference sources) is used, for example, to divert anti-tank guided missiles by means of deployed jammers. Signatures are produced which correspond to the motor of the enemy rockets. The motor is continuously measured in order to control the rockets from the launching apparatus, and the deviation from the expected flight path is carried out by correction of the rockets. This guidance mechanism is influenced by the additional signatures. The rockets are deflected from the flight path.
Jamming can be carried out optically or pyrotechnically. One optical variant is the generation of light flashes by means of a stroboscopic lamp which is fitted in a stationary position on the vehicle. One pyrotechnic variant is pyrotechnic burning in the relevant spectral band by means of a pyrotechnic flare, similar to a Bengal flare.
When pyrotechnic solutions are present in the munitiorl, the jamming is produced by the same munition that is also used to produce the visual blockade (smoke). Light flashes are generated by means of an appropriate break-up charge, integrated in the smoke muriition (DE 38 35 887 C2; DE 28 42 797 C2; DE 10 2005 020 159 A1).
DE 10 2005 054 275 Al describes a self-defence installation for combat vehicles or other objects to be protected. The launch system of the self-defence insta1lation is in this case fitted primarily with a W.BU.0322.WO/DIE - -pyrotechnic munition, in which irritation bodies are included which, immediately after release, produce a powerful light flash and/or smoke. A smoke munition is added to the irritation bodies, for this purpose.
~
J
EP 0 512 202 A2 discloses a method for protection of objects which emit IR radiation, in which, after the missile has been located, a large-area pyrotechnic jamming radiation cloud is produced between the missile and the objet, which cloud first of all briefly emits powerful infrared radiation, which itself interferes with the lock-on and tracking electronics of the homing head. This jamming radiation cloud then emits weak infrared radiation for a comparatively long time. Only after this are a plurality of spoof target clouds created, which deflect the missile step-by-step away from the object to be protected.
The disadvantages of the optical solutions are the high level of technical complexity, the heavy weight and the long firing chain before they become effective.
In the case of pyrotechnic solutions, it has been found that, because of the relatively large munition caliber, it is possible to store and to carry in the vehicle only ammunition for a few missions. Furthermore, the munition is heavy. Furthermore, the ammunition consumption is high because of the normal false-alarm rate.
Conventionally, the munition is fired in the threat direction. This generally depends on alignment of the munition launching installation (DE 10 2005 020 177 A1), which can result in a time delay. A plurality of installatiorls are often necessary in order to allow all threat directions to be covered at the same time (DE 10 2005 054 275 Al).
Vu . i~u . 0~__~ . WG / DT F - ~
Known munition launch installations frequently require a large amount of space and are often difficult to integrate, in particular in vehicles.
A further disadvantage is the muni_tiori itself. 'The functions of jamming and camouflage, for example by means of smoke, are in gerieral always deployed together by this munition. However, smoke iri particular is riot always desirable since it carl impede one's own view.
The invention is based on the object of improved jamming associated with an improved integration capability, by saving weight in the launch installation.
The object is achieved by the features of patent claim 1, patent claim 4 and patent claim 6.
Advantageous embodiments are specified in the dependent claims.
The invention is based on the idea of absolute separation of the functions of camouflage and jamming.
This makes it possible to use a small-caliber munition which deploys exclusively jammers. These jammers or munitions are preferably fired vertically in height and/or laterally by the vehicle (object) to be protected. For this purpose, the launch barrels are fitted and aligned vertically on the vehicle or the object to be protected. Arl adequate light flash is produced in the relevant spectrum by initiation of a pyrotechnic charge, which irlitiat.ion is clocked in time and is arranged offset in height, and the light flash irlterferes with the aiming mechanism of the approaching warhead. Alternatively, different heights of the break-up flashes above and/or to the side of the object can be generated by a plurality of munitions.
W.BU.0322.W0/DIE - 4 -This measure for deployment of the jammers is deployed separately from other effects, such as smoke. The smoke munition, which can be fired separately, then does riot itself need to carry out jamming. This allows a plurality of smoke bodies to be included in the actual smoke munition.
Launching is carried out electrically or mechanically, initiated by a small, compact launching apparatus, for example from magazines. The sub-clocking for initiation of the individual light flashes is controlled by electronics. These electronics are preferably a component of the launching apparatus.
The advantages which result from this are a small launch design, with no aiming elements being required, and lower weight associated with this. Because of the lack of aiming elements, simple integration and a simple technical implementation are possible.
The invention will be explained in more detail using one exemplary embodiment and with reference to the drawing, iri which:
Figure 1 shows a launcher with a munition, Figure 2 shows the munition from Figure 1, and Figure 3 shows an integration optiori on/to a vehicle.
Figure 1 shows a compact launching apparatus or a launcher 1_ in a transparent form, preferably with a plurality of launch barrels 2 which are aligned upward parallel and form a magazine 3. One munition 4 is located in each of these launch barrels 2.
Figure 2 shows the design of the munitions 4. The munition 4 comprises a casing 5 from which one or more W.BU.0322.W0/DIE - 5 -sub-munitioris 6(jammers) are fired. Alternatively, the sub-munitions 6 (jammers) can be fired directly from the magazine 3, without a casing. The munition 4 or sub-munitions 6 has/have a comparatively small caliber for vehicle protectiorl muriitions, for example 40 mm (medium caliber).
The munitions 4 or the sub-munitions 6 have interfaces to the launching apparatus 1, via which they are 10 initiated electrically or mechanically. The sub-clocking for initiatiori of the individual light flashes 8 is controlled by electronics 7. These electronics are preferably a component of the launching apparatus 1. In order to initiate the light flash or break-up flash 8, a plurality of sub-munitions 6 and/or a plurality of munitions 4 can be initiated, clocked in time, successively.
The break-up flashes 8 of the jammers 6 are generated spatially above the vehicle 9 (Figure 3) . The break-up height is preferably in the range from about 3 to 15 m above the vehicle 9. In this case, the height rises within the individual light flashes 8. Firing is preferably carried out from the vehicle 9 vertically upward. A lateral break-up can thus be set, with the break-up taking place with decreasing height.
Figure 3 shows an example of an arrangement of a launching apparatus 1 on a vehicle 9. The break-up flashes 8 are generated at heights of, for example, 4 m, 8 m, or 12 rn above the vehicle 9.
Claims (10)
1. A method for protection of an object (9) against a threat, in particular a missile, by interference, wherein one or more sub-munitions (6) or jammers is or are deployed directly or by means of a munition (4) vertically and/or sideways with respect to the object (9) from a launching apparatus (1), sub-clocking is carried out electronically in order to release the individual sub-munitions (6) and, associated with this, the light flashes (8), as a result of which at least one light flash (8) is produced in the relevant spectrum, which interferes with the aiming mechanism of the threat, and the light flashes (8) are generated with various height and/or lateral offsets with respect to the object (9).
2. The method as claimed in claim 1, characterized in that different heights and/or sides of the break-up flashes can be generated above and/or to the side of the object (9) by a plurality of munitions (4).
3. The method as claimed in claim 1 or 2, characterized in that the break-up height of the sub-munitions is in the range from about 1 to 15 m above the object (9).
4. The method as claimed in one of claims 1 to 3, characterized in that the height rises within the individual light flashes (8).
5. The method as claimed in one of claims 1 to 3, characterized in that the height falls within the individual light flashes (8).
6. A launching apparatus (1) for sub-munitions (6) or a munition (4) having sub-munitions (6) for jamming for projection of an object (9) against a threat, in particular a missile, by interference, comprising launch barrels (2) which are aligned vertically upward, parallel to one another, on the object (9), wherein sub-clocking is carried out electronically in order to release the individual sub-munitions (6) and, associated with this, light flashes (8), and the light flashes (8) are generated with different height and/or lateral offsets with respect to the object (9).
7. The launching apparatus as claimed in claim 5, characterized in that munitions (4) or the sub-munitions (6) have interfaces (10) to the launching apparatus (1), via which they are initiated electrically or mechanically.
8. A munition (4) for protection of objects (9) against a threat, in particular a missile, by interference, comprising one or more sub-munitions (6) or jammers, wherein sub-clocking is carried out electronically in order to release the individual sub-munitions (6) and, associated with this, light flashes (8), and the light flashes (8) are generated with different height and/or lateral offsets with respect to the object (9).
9. The munition as claimed in claim 7, characterized in that the munition is fired directly, without a casing, from a magazine (3) or a launch barrel (2).
10. The munition as claimed in claim 7 or 8, characterized in that the munition (4) or sub-munitions (6) has/have a comparatively small caliber for vehicle protection munitions.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102007032112.2 | 2007-07-09 | ||
| DE102007032112A DE102007032112A1 (en) | 2007-07-09 | 2007-07-09 | Method and launcher for protecting an object from a threat, in particular a missile, and ammunition |
| PCT/EP2008/004858 WO2009006981A1 (en) | 2007-07-09 | 2008-06-17 | Method and launching apparatus for protection of an object against a threat, in particular a missile, as well as munition |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2693006A1 true CA2693006A1 (en) | 2009-01-15 |
Family
ID=39789913
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA 2693006 Abandoned CA2693006A1 (en) | 2007-07-09 | 2008-06-17 | Method and launching apparatus for protection of an object against a threat, in particular a missile, as well as munition |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US20100288111A1 (en) |
| EP (1) | EP2165151A1 (en) |
| JP (1) | JP2010532857A (en) |
| KR (1) | KR20100049033A (en) |
| AU (1) | AU2008274621A1 (en) |
| BR (1) | BRPI0813697A2 (en) |
| CA (1) | CA2693006A1 (en) |
| DE (1) | DE102007032112A1 (en) |
| WO (1) | WO2009006981A1 (en) |
| ZA (1) | ZA200909071B (en) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102009020558A1 (en) | 2009-05-08 | 2010-11-18 | Rheinmetall Waffe Munition Gmbh | Activation unit for ammunition-free decoys |
| DE102008028245A1 (en) | 2008-06-16 | 2009-12-17 | Rheinmetall Waffe Munition Gmbh | Flare Ignition and use in an exhaust system |
| KR20120014134A (en) | 2009-05-08 | 2012-02-16 | 라인메탈 바페 뮤니션 게엠베하 | Activation unit for explosive masses or explosive bodies |
| DE102009020557B4 (en) * | 2009-05-08 | 2011-03-31 | Rheinmetall Waffe Munition Gmbh | Activation unit for active substances or active bodies |
| DE102009030870A1 (en) | 2009-06-26 | 2010-12-30 | Rheinmetall Waffe Munition Gmbh | submunitions |
| DE102009030869A1 (en) | 2009-06-26 | 2011-02-10 | Rheinmetall Waffe Munition Gmbh | submunitions |
| DE102012010378A1 (en) * | 2012-05-29 | 2013-12-05 | Rheinmetall Waffe Munition Gmbh | Ammunition with active agents |
| DE102012010377A1 (en) * | 2012-05-29 | 2013-12-05 | Rheinmetall Waffe Munition Gmbh | Ammunition with active agents |
Family Cites Families (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3841219A (en) * | 1964-08-12 | 1974-10-15 | Gen Dynamics Corp | Decoy rounds for counter measures system |
| US3808940A (en) * | 1964-12-24 | 1974-05-07 | Gen Dynamics Corp | Portable decoy launcher system and rounds therefor |
| US4307665A (en) * | 1965-12-21 | 1981-12-29 | General Dynamics Corporation | Decoy rounds |
| US4063485A (en) * | 1966-12-21 | 1977-12-20 | General Dynamics Corporation | Decoy launcher system |
| US4178854A (en) * | 1967-12-22 | 1979-12-18 | General Dynamics Corporation, Pomona Division | Multiple sequential burst system |
| US3708563A (en) * | 1970-09-21 | 1973-01-02 | Sells Inc | Magazine for aerial dispenser and method of making same |
| US4135455A (en) * | 1977-02-03 | 1979-01-23 | Tracor, Inc. | Multiple payload cartridge employing single pair of electrical connections |
| FR2383419A1 (en) * | 1977-03-07 | 1978-10-06 | Lacroix E | LURE LAUNCHER CASE FOR WEAPON GUIDANCE SYSTEMS ACCEPTANCE |
| DE2842797C2 (en) | 1978-09-30 | 1986-01-23 | Nico-Pyrotechnik Hans-Jürgen Diederichs KG, 2077 Trittau | Throwing bodies |
| US4195571A (en) * | 1979-04-02 | 1980-04-01 | The United States Of America As Represented By The Secretary Of The Army | Modular wheel dispenser |
| US4305325A (en) * | 1979-10-31 | 1981-12-15 | The United States Of America As Represented By The Secretary Of The Navy | General purpose decoy launcher |
| DE3421734A1 (en) | 1984-06-12 | 1985-12-12 | Buck Chemisch-Technische Werke GmbH & Co, 7347 Bad Überkingen | METHOD FOR PROTECTING INFRARED RADIATING DESTINATIONS, ESPECIALLY SHIPS, FROM AIRCRAFT EQUIPPED WITH INFRARED STEERING HEADS |
| DE3835887C2 (en) | 1988-10-21 | 1997-10-02 | Rheinmetall Ind Ag | Cartridge for creating false targets |
| DE4115384C2 (en) | 1991-05-10 | 1994-07-07 | Buck Chem Tech Werke | Method for protecting objects emitting IR radiation |
| DE4125356C2 (en) * | 1991-07-31 | 1995-07-06 | Buck Chem Tech Werke | Self-protection launcher facility |
| SE469196B (en) * | 1991-10-02 | 1993-05-24 | Nobeltech Electronics Ab | COMMON UNIT AND FAILURE SYSTEM INCLUDING AT LEAST ONE SUCH UNIT |
| FR2692032B1 (en) * | 1992-06-05 | 1994-07-22 | Poudres & Explosifs Ste Nale | MULTI-HOUSING PYROTECHNIC CARTRIDGES AND CORRESPONDING AMMUNITION. |
| US5400690A (en) * | 1992-06-05 | 1995-03-28 | Societe Nationale Des Poudres Et Explosifs | Multi-receptacle pyrotechnic cartridges and corresponding ammunition |
| US5452640A (en) * | 1993-05-06 | 1995-09-26 | Fmc Corporation | Multipurpose launcher and controls |
| US5495787A (en) * | 1994-06-17 | 1996-03-05 | Boyer, Iii; Lynn L. | Anti-missile missiles having means to "blind", and thus render ineffective, precision, seeker guided munitions |
| DE19936587C2 (en) | 1999-08-04 | 2003-08-21 | Buck Neue Technologien Gmbh | Ammunition or pyrotechnic device for deploying submunitions |
| AUPQ413299A0 (en) * | 1999-11-18 | 1999-12-09 | Metal Storm Limited | Forming temporary airborne images |
| SE520197C2 (en) * | 2001-05-07 | 2003-06-10 | Saab Ab | Method for outputting IR and radar countermeasures and / or laser reflectors from a designated trap, and for outputting such countermeasures or reflectors |
| DE102005020177A1 (en) | 2005-04-28 | 2006-11-02 | Rheinmetall Waffe Munition Gmbh | Launch system |
| DE102005020159B4 (en) | 2005-04-29 | 2007-10-04 | Rheinmetall Waffe Munition Gmbh | Camouflage and deception ammunition for the protection of objects against missiles |
| DE102005054275A1 (en) | 2005-11-11 | 2007-05-16 | Rheinmetall Waffe Munition | Self-protection system for combat vehicles or other objects to be protected |
-
2007
- 2007-07-09 DE DE102007032112A patent/DE102007032112A1/en not_active Withdrawn
-
2008
- 2008-06-17 JP JP2010515364A patent/JP2010532857A/en active Pending
- 2008-06-17 US US12/668,365 patent/US20100288111A1/en not_active Abandoned
- 2008-06-17 CA CA 2693006 patent/CA2693006A1/en not_active Abandoned
- 2008-06-17 KR KR1020107001131A patent/KR20100049033A/en not_active Application Discontinuation
- 2008-06-17 AU AU2008274621A patent/AU2008274621A1/en not_active Abandoned
- 2008-06-17 EP EP08759260A patent/EP2165151A1/en not_active Ceased
- 2008-06-17 WO PCT/EP2008/004858 patent/WO2009006981A1/en active Application Filing
- 2008-06-17 BR BRPI0813697-1A2A patent/BRPI0813697A2/en not_active Application Discontinuation
-
2009
- 2009-12-18 ZA ZA2009/09071A patent/ZA200909071B/en unknown
Also Published As
| Publication number | Publication date |
|---|---|
| WO2009006981A1 (en) | 2009-01-15 |
| EP2165151A1 (en) | 2010-03-24 |
| DE102007032112A1 (en) | 2009-01-15 |
| BRPI0813697A2 (en) | 2014-12-30 |
| US20100288111A1 (en) | 2010-11-18 |
| KR20100049033A (en) | 2010-05-11 |
| AU2008274621A1 (en) | 2009-01-15 |
| JP2010532857A (en) | 2010-10-14 |
| ZA200909071B (en) | 2011-11-30 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FZDE | Discontinued |