CA2719374A1 - Active body for a submunition having effective agents - Google Patents
Active body for a submunition having effective agents Download PDFInfo
- Publication number
- CA2719374A1 CA2719374A1 CA2719374A CA2719374A CA2719374A1 CA 2719374 A1 CA2719374 A1 CA 2719374A1 CA 2719374 A CA2719374 A CA 2719374A CA 2719374 A CA2719374 A CA 2719374A CA 2719374 A1 CA2719374 A1 CA 2719374A1
- Authority
- CA
- Canada
- Prior art keywords
- active
- active mass
- insulating layer
- submunition
- mass 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.)
- Abandoned
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
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/56—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
- F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
- F42B12/62—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile
-
- 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
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/42—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information of illuminating type, e.g. carrying flares
-
- 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
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/46—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances
- F42B12/48—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances smoke-producing, e.g. infrared clouds
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Air Bags (AREA)
Abstract
The invention relates to a submunition having effective masses, particularly having at least one pyrotechnic fog body (1), comprising an insulation layer (2) between an active body container (3) and a pyrotechnic unit (4), wherein the active body container (3) can be closed by a cover (5) having a blow-out opening (6).
Description
DESCRIPTION
Active body for a submunition having effective agents The invention relates to a thermal insulating layer in particular between smoke and flare containers.
Infrared-guided, radar-guided and dual-mode-guided missiles are used, inter alia, to attack, for example, seaborne targets, such as marine vessels, or other objects on the land and in the air. After being fired, these missiles or rockets initially fly with inertial assistance (for example DE 196 01 165 Al) or are guided by GPS to the target region. The missile then enters a search phase once it is sufficiently close to the target. Furthermore, the missiles are switched to the target (lock-on) and track this target until impact (track phase) . A "track-gate" depth D is approximately 150 meters in relatively old missiles, and only a few meters in modern missiles.
Various decoy bodies are used to decoy such guided missiles, in order to impede the function of the missiles by jamming or interference, in order to protect objects. When a threat is identified, some decoy bodies emit electromagnetic decoy signals (DE 100 16 781 C2), and others form "clouds" of floating dipoles (chaff clouds), which are matched to the radar frequency of the missile.
Pyrotechnic objects are ejected as submunition from a projectile at a specific altitude and are initiated in the process, before they then fall to the ground as they burn.
However, conventional submunitions occasionally have the disadvantage that heating can result in uncontrollable separation of the active mass from the active mass container, which could lead to uncontrolled involvement in the exothermic reaction of the active mass in the system.
Until now, the aim of achieving an active mass assembly of greater strength has been attempted by greater compression forces during manufacture.
EP 1 026 473 discloses a method for providing a decoy target for protection of land vehicles, aircraft or watercraft or the like, in which the missiles have a target seeker head which operates in the infrared band or radar band, or a target seeker head which operates in both wavelength bands at the same time or successively. In this case, the RF active mass in the form of dipole packs, in particular, is protected by a heat shield against the blow-out heat.
The object of the invention here is to specify a submunition with active masses which avoids the abovementioned disadvantages and in which the functional reliability of the active masses is considerably improved.
The invention is based on the idea of including an insulating layer, in particular a thermal insulating layer, between the submunitions to prevent the heat development that results from deliberate combustion of the active masses and the heat transfer which then follows via the active mass container to active mass layers located underneath. The insulating layer is fitted in/on the active mass container by pushing in, insertion, injection and/or application, after which filling with the active mass takes place. This ensures that a minimum amount of heat is introduced into the active mass that has not yet been burnt, as a result of the heat transfer during combustion. Flashover and explosive combustion are prevented. The separation of the active mass from the container prevents heat being introduced from the container to the active mass, and/or a reaction from the container on the active mass, during combustion.
One advantage associated with this is that this layer has a shock-absorbing effect and is therefore suitable for minimizing the force/impulse introduced to the active mass as a result of striking the ground. At the same time, the insulating layer prevents the active mass from falling out as a result of strength losses, in particular resulting from heat development.
Preparations or products of non-toxic, organic or inorganic compounds from groups 2, 3 and 4 of the periodic table of the elements, such as magnesium, calcium, boron, aluminum, carbon, silicon and tin, are preferably used, that is to say compounds whose chemical and physical characteristics comply with the characteristic preconditions of an insulating layer are used, as the basis for the insulating layer.
The inclusion of an insulating layer therefore improves the functional reliability by initiation of uniform combustion of the active mass until completion of burning, and, associated with this, improves a more uniform function by the active bodies, as well as improving safety with regard to objects thrown out during explosive combustion.
The invention will be explained in more detail with reference to one exemplary embodiment and a drawing.
The single figure shows the basic design of a pyrotechnic smoke body 1 having an insulating layer 2 between the active body container 3 and the pyrotechnic charge 4. The active body containers 3 are distributed symmetrically around an imaginary projectile longitudinal axis 10. A plurality of active body containers 3 can form a submunition to be fired (not illustrated in any more detail). The container 3 or the housing can be closed by a cover 5 with a blow-out opening 6.
Active body for a submunition having effective agents The invention relates to a thermal insulating layer in particular between smoke and flare containers.
Infrared-guided, radar-guided and dual-mode-guided missiles are used, inter alia, to attack, for example, seaborne targets, such as marine vessels, or other objects on the land and in the air. After being fired, these missiles or rockets initially fly with inertial assistance (for example DE 196 01 165 Al) or are guided by GPS to the target region. The missile then enters a search phase once it is sufficiently close to the target. Furthermore, the missiles are switched to the target (lock-on) and track this target until impact (track phase) . A "track-gate" depth D is approximately 150 meters in relatively old missiles, and only a few meters in modern missiles.
Various decoy bodies are used to decoy such guided missiles, in order to impede the function of the missiles by jamming or interference, in order to protect objects. When a threat is identified, some decoy bodies emit electromagnetic decoy signals (DE 100 16 781 C2), and others form "clouds" of floating dipoles (chaff clouds), which are matched to the radar frequency of the missile.
Pyrotechnic objects are ejected as submunition from a projectile at a specific altitude and are initiated in the process, before they then fall to the ground as they burn.
However, conventional submunitions occasionally have the disadvantage that heating can result in uncontrollable separation of the active mass from the active mass container, which could lead to uncontrolled involvement in the exothermic reaction of the active mass in the system.
Until now, the aim of achieving an active mass assembly of greater strength has been attempted by greater compression forces during manufacture.
EP 1 026 473 discloses a method for providing a decoy target for protection of land vehicles, aircraft or watercraft or the like, in which the missiles have a target seeker head which operates in the infrared band or radar band, or a target seeker head which operates in both wavelength bands at the same time or successively. In this case, the RF active mass in the form of dipole packs, in particular, is protected by a heat shield against the blow-out heat.
The object of the invention here is to specify a submunition with active masses which avoids the abovementioned disadvantages and in which the functional reliability of the active masses is considerably improved.
The invention is based on the idea of including an insulating layer, in particular a thermal insulating layer, between the submunitions to prevent the heat development that results from deliberate combustion of the active masses and the heat transfer which then follows via the active mass container to active mass layers located underneath. The insulating layer is fitted in/on the active mass container by pushing in, insertion, injection and/or application, after which filling with the active mass takes place. This ensures that a minimum amount of heat is introduced into the active mass that has not yet been burnt, as a result of the heat transfer during combustion. Flashover and explosive combustion are prevented. The separation of the active mass from the container prevents heat being introduced from the container to the active mass, and/or a reaction from the container on the active mass, during combustion.
One advantage associated with this is that this layer has a shock-absorbing effect and is therefore suitable for minimizing the force/impulse introduced to the active mass as a result of striking the ground. At the same time, the insulating layer prevents the active mass from falling out as a result of strength losses, in particular resulting from heat development.
Preparations or products of non-toxic, organic or inorganic compounds from groups 2, 3 and 4 of the periodic table of the elements, such as magnesium, calcium, boron, aluminum, carbon, silicon and tin, are preferably used, that is to say compounds whose chemical and physical characteristics comply with the characteristic preconditions of an insulating layer are used, as the basis for the insulating layer.
The inclusion of an insulating layer therefore improves the functional reliability by initiation of uniform combustion of the active mass until completion of burning, and, associated with this, improves a more uniform function by the active bodies, as well as improving safety with regard to objects thrown out during explosive combustion.
The invention will be explained in more detail with reference to one exemplary embodiment and a drawing.
The single figure shows the basic design of a pyrotechnic smoke body 1 having an insulating layer 2 between the active body container 3 and the pyrotechnic charge 4. The active body containers 3 are distributed symmetrically around an imaginary projectile longitudinal axis 10. A plurality of active body containers 3 can form a submunition to be fired (not illustrated in any more detail). The container 3 or the housing can be closed by a cover 5 with a blow-out opening 6.
Claims (6)
1. An active mass body for a submunition having active masses, in particular a pyrotechnic smoke body (1), having an effective agent body container (3) and a pyrotechnic charge (4), characterized in that an insulating layer (2) is included between the active body container (3) and the pyrotechnic charge (4), and the active body container (3) can be closed by a cover (5) with a blow-out opening (6).
2. The active mass body as claimed in claim 1, characterized in that a plurality of smoke bodies (1) form the submunition.
3. The active mass body as claimed in claim 2, characterized in that the active body containers (3) are distributed symmetrically around an imaginary projectile longitudinal axis (10).
4. The active mass body as claimed in one of claims 1 to 3, characterized in that compounds whose chemical and physical characteristics comply with the characteristic preconditions of an insulating layer are used as the basis for the insulating layer (2).
5. The active mass body as claimed in claim 4, characterized in that preparations or products of non-toxic, organic or inorganic compounds from groups 2, 3 and 4 of the periodic table of the elements, such as magnesium, calcium, boron, aluminum, carbon, silicon and tin, are preferably used.
6. The active mass body as claimed in one of claims 1 to 5, characterized in that the insulating layer (2) has a shock-absorbing effect.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102008019752A DE102008019752A1 (en) | 2008-04-18 | 2008-04-18 | Active body for a submunition with active agents |
DE102008019752.1 | 2008-04-18 | ||
PCT/EP2009/002070 WO2009127309A1 (en) | 2008-04-18 | 2009-03-20 | Active body for a submunition having effective agents |
Publications (1)
Publication Number | Publication Date |
---|---|
CA2719374A1 true CA2719374A1 (en) | 2009-10-22 |
Family
ID=40846973
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA2719374A Abandoned CA2719374A1 (en) | 2008-04-18 | 2009-03-20 | Active body for a submunition having effective agents |
Country Status (5)
Country | Link |
---|---|
US (1) | US20110088582A1 (en) |
EP (1) | EP2265892A1 (en) |
CA (1) | CA2719374A1 (en) |
DE (1) | DE102008019752A1 (en) |
WO (1) | WO2009127309A1 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102011100243A1 (en) | 2011-05-02 | 2012-11-08 | Rheinmetall Waffe Munition Gmbh | Active mass container |
DE102017122351A1 (en) | 2017-09-26 | 2019-03-28 | Rheinmetall Waffe Munition Gmbh | mist body |
DE102017122350A1 (en) | 2017-09-26 | 2019-03-28 | Rheinmetall Waffe Munition Gmbh | mist body |
DE102017122352A1 (en) | 2017-09-26 | 2019-03-28 | Rheinmetall Waffe Munition Gmbh | mist body |
DE102018129786B4 (en) * | 2018-11-26 | 2022-03-03 | Rheinmetall Waffe Munition Gmbh | Test and/or practice ammunition |
Family Cites Families (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1366555A (en) * | 1918-12-30 | 1921-01-25 | Brayton Harold Morgan | Illuminating-shell |
US3238143A (en) * | 1963-08-16 | 1966-03-01 | Robert L Ainsley | Aerosol generators |
SE312086B (en) * | 1968-06-10 | 1969-06-30 | Bofors Ab | |
US4062709A (en) * | 1968-09-25 | 1977-12-13 | Castaneda Victor F | Inhibited fluorocarbon rocket propellant |
GB1277528A (en) * | 1970-10-21 | 1972-06-14 | Thiokol Chemical Corp | Illuminating flare and method of producing the same |
DE2359758C1 (en) * | 1973-11-30 | 1988-07-28 | Buck Chemisch-Technische Werke Gmbh & Co, 7347 Bad Ueberkingen, De | |
US3983816A (en) * | 1974-01-16 | 1976-10-05 | Thiokol Corporation | Compositions for producing flickering signals |
DE2437535C3 (en) * | 1974-08-03 | 1981-08-06 | Rheinmetall GmbH, 4000 Düsseldorf | Ejectable smoke pot for highly stressed projectiles |
DE2525553A1 (en) * | 1975-06-07 | 1976-12-23 | Rheinmetall Gmbh | EXHAUSTABLE PAYLOAD FOR HIGHLY DEMANDED STORIES |
DE2555323C2 (en) * | 1975-12-09 | 1984-04-05 | Buck Chemisch-Technische Werke GmbH & Co, 7341 Bad Überkingen | Projectile filling from smoke pots arranged on top of one another and method for the production of a smoke pot |
DE2811016C1 (en) * | 1978-03-14 | 1986-07-17 | Buck Chemisch-Technische Werke Gmbh & Co, 8230 Bad Reichenhall | Throwing body |
US4860657A (en) * | 1978-05-05 | 1989-08-29 | Buck Chemisch-Technische Werke Gmbh & Co. | Projectile |
DE2841815C2 (en) * | 1978-09-26 | 1985-02-21 | Buck Chemisch-Technische Werke GmbH & Co, 7347 Bad Überkingen | Method for producing a floor filling |
US4791870A (en) * | 1983-04-05 | 1988-12-20 | Haley & Weller Limited | Pyrotechnic assembly |
US4881464A (en) * | 1989-03-06 | 1989-11-21 | The United States Of America As Represented By The Secretary Of The Army | Signal or rescue flare of variable luminosity |
USH699H (en) * | 1989-07-10 | 1989-11-07 | The United States Of America As Represented By The Secretary Of The Army | Submunition fuse with pyrotechnic ignition |
DE3934362A1 (en) * | 1989-10-14 | 1991-04-18 | Rheinmetall Gmbh | BOMBLET CARRIER FLOOR WITH LIGHTLY EXERCISED BOMBLETS |
NO176495C (en) * | 1993-02-03 | 1995-04-19 | Raufoss As | Device by smoke grenade |
DE19601165A1 (en) | 1996-01-15 | 1997-07-17 | Bodenseewerk Geraetetech | Decoys for deflecting aiming guided missiles |
DE19617701C2 (en) | 1996-05-03 | 2000-01-13 | Buck Werke Gmbh & Co I K | Method of providing a dummy target |
US5983801A (en) * | 1998-04-29 | 1999-11-16 | Brunn; Michael | Separating smoke grenade |
DE10016781C2 (en) | 2000-04-05 | 2003-07-03 | Eads Deutschland Gmbh | guard |
DE10105867B4 (en) * | 2001-02-09 | 2004-03-04 | Buck Neue Technologien Gmbh | bullet |
US20030056680A1 (en) * | 2001-09-25 | 2003-03-27 | Falken, S.A. | Device with combustible charge with smoke-generating, tear-generating or signaling effects |
DE10249920A1 (en) * | 2002-10-26 | 2004-05-13 | Diehl Munitionssysteme Gmbh & Co. Kg | Smoke grenade comprises sleeve, ogive fixed to it, base and timed detonator connected to charge |
DE10308307B4 (en) * | 2003-02-26 | 2007-01-04 | Buck Neue Technologien Gmbh | Projectile and submunition with preload body |
DE102007057184A1 (en) * | 2007-11-26 | 2009-05-28 | Rheinmetall Waffe Munition Gmbh | Ammunition or missile for battlefield lighting |
-
2008
- 2008-04-18 DE DE102008019752A patent/DE102008019752A1/en not_active Withdrawn
-
2009
- 2009-03-20 WO PCT/EP2009/002070 patent/WO2009127309A1/en active Application Filing
- 2009-03-20 EP EP09733587A patent/EP2265892A1/en not_active Withdrawn
- 2009-03-20 CA CA2719374A patent/CA2719374A1/en not_active Abandoned
-
2010
- 2010-10-18 US US12/906,898 patent/US20110088582A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
US20110088582A1 (en) | 2011-04-21 |
DE102008019752A1 (en) | 2009-10-22 |
WO2009127309A1 (en) | 2009-10-22 |
EP2265892A1 (en) | 2010-12-29 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US6513438B1 (en) | Method for offering a phantom target, and decoy | |
US5835051A (en) | Method for offering a phantom target | |
US6957602B1 (en) | Parachute active protection apparatus | |
US8387540B2 (en) | Interceptor projectile and method of use | |
RU2275585C2 (en) | Method for control of missile flight direction and missile | |
US7104496B2 (en) | Active protection device and associated apparatus, system, and method | |
US4406227A (en) | System for multistage, aerial dissemination and rapid dispersion of preselected substances | |
CA2554839C (en) | Active protection device and associated apparatus, system, and method | |
US10731950B2 (en) | Vehicle defense projectile | |
CN112179213B (en) | Missile interception method, memory and server | |
US20110088582A1 (en) | Active body for a submunition having effective agents | |
US7387060B1 (en) | Rocket exhaust defense system and method | |
US5841059A (en) | Projectile with an explosive load triggered by a target-sighting device | |
AU695538B2 (en) | Method for protecting objects, especially ships, that emit a radiation, particularly infrared radiation, against missiles | |
RU203385U1 (en) | Incendiary fragmentation projectile | |
RU2377493C2 (en) | Method of hitting vulnerable ground targets by supersonic missile and device to this effect | |
Burt | The cruise missile and arms control | |
IL169423A (en) | Warhead for artillery ammunition | |
EP0791800B1 (en) | Anti-missile missiles | |
RU206148U1 (en) | Incendiary fragmentation projectile | |
RU2777149C1 (en) | Complex for active protection of armored vehicles | |
PL225266B1 (en) | System of active defense | |
RU2255296C2 (en) | Device for set-up of wide-band jamming | |
RU221614U1 (en) | ANTI-SHIP MISSILE WARNING UNIT | |
RU2034232C1 (en) | Directive fragmentation shell cluster |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FZDE | Discontinued |
Effective date: 20150320 |