DE102005024179A1 - Method and device for temping and / or correction of the ignition timing of a projectile - Google Patents
Method and device for temping and / or correction of the ignition timing of a projectile Download PDFInfo
- Publication number
- DE102005024179A1 DE102005024179A1 DE102005024179A DE102005024179A DE102005024179A1 DE 102005024179 A1 DE102005024179 A1 DE 102005024179A1 DE 102005024179 A DE102005024179 A DE 102005024179A DE 102005024179 A DE102005024179 A DE 102005024179A DE 102005024179 A1 DE102005024179 A1 DE 102005024179A1
- Authority
- DE
- Germany
- Prior art keywords
- projectile
- weapon
- correction
- calculation
- transmitter
- 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.)
- Withdrawn
Links
Classifications
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C11/00—Electric fuzes
- F42C11/06—Electric fuzes with time delay by electric circuitry
- F42C11/065—Programmable electronic delay initiators in projectiles
Abstract
Description
Die Erfindung betrifft ein Verfahren und eine Vorrichtung für das Programmieren eines tempierbaren Geschosses bzw. zur Korrektur eines Zündzeitpunktes eines aus einer Waffe verschossenen Geschossses.The The invention relates to a method and apparatus for programming a malleable projectile or for the correction of an ignition point a missile fired from a weapon.
Es
sind verschiedene Zeitprogrammierungen für Munitionen bekannt. Die Tempierungen
erfolgen entweder vor dem Schuss manuell außerhalb des Ladungsraums oder
elektrisch im Ladungsraum über
eine Anzündelektronik.
Letztgenannte Tempierung ist beispielsweise in der
Ein
Verfahren und eine Vorrichtung zur Übertragung von Informationen
auf programmierbare Geschosse sind der
Ein
Verfahren zum Korrigieren einer vorprogrammierten Auslösung eines
Vorganges in einem drallstabilisierten Geschoss sowie eine Vorrichtung zur
Durchführung
des Verfahrens werden in der
In
der
Ein
Verfahren und eine Vorrichtung zum Programmieren von Zeitzündern von
Geschossen werden auch in der
Aus
der
Aus
der
Die vorgenannte Vorrichtung zeichnet sich zwar durch eine hohe Genauigkeit aus, unterliegt jedoch mechanischen und thermodynamischen Belastungen, da die Mess- und Programmiereinheit u. a. den Mündungsgasen ausgesetzt sind.The Although the aforementioned device is characterized by high accuracy but is subject to mechanical and thermodynamic loads, since the measuring and programming unit u. a. are exposed to the muzzle gases.
Hier greift die Erfindung die Aufgabe auf, eine Vorrichtung bzw. ein verbessertes Programmiersystem aufzuzeigen, welches keinem mechanischen und thermodynamischen Verschleiß mehr ausgesetzt ist.Here the invention addresses the problem of a device or a Improved programming system to show that no mechanical and thermodynamic wear more is exposed.
Gelöst wird die Aufgabe durch die Merkmale des Patentanspruchs 1 bzw. des Patentanspruchs 5, wobei Anspruch 1 ein Verfahren und Anspruch 5 eine Vorrichtung beanspruchen.Is solved the object by the features of claim 1 or the claim 5, wherein claim 1 is a method and claim 5 a device claim.
Vorteilhafte Ausführungen sind in den Unteransprüchen enthalten.advantageous versions are in the subclaims contain.
Der Erfindung liegt die Idee zugrunde, die Vorteile der Messung einer Mündungsgeschwindigkeit und einer aktuellen kompensierten Tempierung beibehaltend, einen Mikrowellensender, vorzugsweise im GHz-Bereich, ins System einzubinden, der die aktuelle, beispielsweise von einem Feuerleitrechner bestimmte Tempierung an eine Munition bzw. ein Geschoss sendet. Auf eine direkte Messung der aktuellen Mündungsgeschwindigkeit kann verzichtet werden, da die reale Mündungsgeschwindigkeit durch Information der aktuellen Fluggeschwindigkeit des Geschosses bestimmt, d.h., aus dieser zurückgerechnet wird. Anhand dieser aktuellen Geschossgeschwindigkeit wird dann die Zündzeit des Geschosses mit Hilfe einer Norm-Mündungsgeschwindigkeit voreingestellte Zündzeit korrigiert und als aktuelle Zünderstellzeit verwendet.Of the Invention is based on the idea of the advantages of measuring a muzzle velocity and maintaining a current compensated temp, one Microwave transmitter, preferably in the GHz range, to be integrated into the system, the current, for example, determined by a fire control computer Temping sends to an ammunition or a projectile. On a direct Measurement of the current muzzle velocity can be dispensed with, because the real muzzle velocity by information the actual airspeed of the projectile, i.e. calculated back from this becomes. Based on this current bullet speed is then the ignition time of the projectile with the aid of a standard muzzle velocity ignition corrected and as the current ignition timing used.
Die Messung der Fluggeschwindigkeit erfolgt beispielsweise mittels Dopplerverschiebung der Sendefrequenzen vorzugsweise geschossseitig. Dazu wird die Sendefrequenz fest eingestellt und die Abweichung gemessen. Da die Zeit bekannt ist, die das Geschoss jeweils zurückgelegt hat, kann die aktuelle Fluggeschwindigkeit bestimmt und zudem die reale Mün dungsgeschwindigkeit des Geschosses, die das Geschoss zum Zeitpunkt der Abschusses durch den Mündungsbereich besessen hat, errechnet werden. Aus diesen Daten wird dann die aktuelle Zünderstellzeit ermittelt und dem Geschoss zur Verfügung gestellt.The Measurement of the airspeed is done for example by means of Doppler shift the transmission frequencies preferably on the storey side. This is the transmission frequency fixed and the deviation measured. As the time known is, which has completed the projectile each, the current airspeed determines and also the real coin speed of the projectile that passed through the projectile at the time of the launch the mouth area has been calculated. From this data is then the current Fuse setting time determined and made available to the projectile.
Bei einer Abweichung von einer vorprogrammierten Norm-Tempierung wird in der Munition oder durch die Feuerleitanlage eine Korrektur vorgenommen, die dann die aktuelle Zünderstellzeit widerspiegelt.In case of a deviation from a pre-programmed standard temping is in the ammunition or a correction made by the fire control system, which then reflects the current ignition timing.
In der Munition bzw. im Geschoss befindet sich für die Programmierung ein Chip, beispielsweise ein RFID (Radio Frequenz Identifikation) – Chip (siehe http://de.wikipedia.org/wiki/RFID). Dieser weist die bevorzugte Eigenschaft auf, dass er über die Mikrowellenstrahlung mit Energie versorgt werden kann.In the ammunition or in the projectile is a chip for programming, For example, an RFID (Radio Frequency Identification) chip (see http://de.wikipedia.org/wiki/RFID). This one has the preferred one Property on that he over the microwave radiation can be powered.
Des Weiteren ergibt sich ein Vorteil daraus, dass der Chip u. a. mit der aktuellen Norm-Tempierung als auch mit einem Korrekturwert oder einem erst während des Fluges ermittelten Wert vom Feuerleitgerät programmierbar ist.Of Furthermore, there is an advantage that the chip u. a. With the current standard temp as well as with a correction value or only during the Flight determined value from the fire control is programmable.
Der an der Munition (bzw. in der Munition) befindliche Timer kann dann über die (verbleibende) Flugstrecke bis Null heruntergezählt und dann die gewollte Zerlegung vor einem Ziel bewerkstelligen.Of the on the ammunition (or in the ammunition) located timer can then on the count down (remaining) flight distance to zero and then the desired decomposition accomplish before a goal.
Zusätzlich kann die berechnete Mündungsgeschwindigkeit auch zurückgesendet werden, wenn diese Berechnung im Geschoss erfolgt, um eventuelle Abweichungen in der Feuerleitung berücksichtigen zu können.In addition, can the calculated muzzle velocity also sent back If this calculation is made on the floor, then any To be able to take into account deviations in the fire line.
Durch dieses System fällt in der Kanone bzw. im Waffenrohr die bisher bekannte aufwändige Mess- und Programmiereinheit weg. Der verwendete Mikrowellensender ist örtlich am Geschütz befestigbar, wo er weder Mündungsgasen noch mechanischen Belastungen ausgesetzt ist. Der Sender/Empfänger wird elektrisch von der Geschützelektrik versorgt und mit Daten der Feuerleitung versorgt. Eventuell von der Munition zurückgesendete Daten können an die Feuerleitung weitergeleitet und von dieser berücksichtigt werden.By this system falls in the cannon or in the barrel the previously known elaborate measuring and Programming unit away. The used microwave transmitter is locally at gun attachable, where he neither mouth gases is still exposed to mechanical stress. The transmitter / receiver becomes electrically from the gun electrical system supplied and supplied with data of the fire control. Maybe from the Ammunition returned Data can forwarded to the fire control and considered by this become.
Anhand eines Ausführungsbeispiels mit Zeichnung soll die Erfindung näher erläutert werden.Based an embodiment with drawing, the invention will be explained in more detail.
Es
zeigt die einzige Figur ein Programmiersystem
An
Bord des Geschosses
Die
Energieversorgung zu den Baugruppen des Geschosses
Geschütz- bzw.
waffenseitig
Die
Funktionsweise ist wie folgt:
Die aktuelle Zerlegungszeit,
berechnet nach der Normgeschwindigkeit des Geschosses
The current decomposition time, calculated according to the standard velocity of the projectile
Erfolgt
dies im Geschoss
Wird
hingegen die aktuelle Geschossgeschwindigkeit an den Sender/Empfänger
Claims (9)
Priority Applications (10)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102005024179A DE102005024179A1 (en) | 2005-05-23 | 2005-05-23 | Method and device for temping and / or correction of the ignition timing of a projectile |
DK06002014.6T DK1726911T3 (en) | 2005-05-23 | 2006-02-01 | Method and apparatus for tempering and / or correcting the detonation time of a projectile |
AT06002014T ATE506594T1 (en) | 2005-05-23 | 2006-02-01 | METHOD AND DEVICE FOR TEMPERATING AND/OR CORRECTING THE IGNITION TIME OF A BULLET |
EP06002014A EP1726911B1 (en) | 2005-05-23 | 2006-02-01 | Method and device for time setting and for correcting the ignition time in a projectile |
ES06002014T ES2365039T3 (en) | 2005-05-23 | 2006-02-01 | PROCEDURE AND DEVICE FOR THE PROGRAMMING OF TIME AND / OR CORRECTION OF THE MOMENT OF THE IGNITION OF A PROJECT. |
DE502006009327T DE502006009327D1 (en) | 2005-05-23 | 2006-02-01 | Method and device for temping and / or correction of the ignition timing of a projectile |
CA002545300A CA2545300A1 (en) | 2005-05-23 | 2006-04-28 | Method and device for setting the fuse and/or correcting the ignition time of a projectile |
US11/436,327 US20070074625A1 (en) | 2005-05-23 | 2006-05-18 | Method and device for setting the fuse and/or correcting the ignition time of a projectile |
JP2006140346A JP5005954B2 (en) | 2005-05-23 | 2006-05-19 | Method and apparatus for setting shell fuze and / or correcting ignition timing |
ZA200604101A ZA200604101B (en) | 2005-05-23 | 2006-05-22 | Method and device for setting the fuse and/or correcting the ignition time of a projectile |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102005024179A DE102005024179A1 (en) | 2005-05-23 | 2005-05-23 | Method and device for temping and / or correction of the ignition timing of a projectile |
Publications (1)
Publication Number | Publication Date |
---|---|
DE102005024179A1 true DE102005024179A1 (en) | 2006-11-30 |
Family
ID=35901540
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE102005024179A Withdrawn DE102005024179A1 (en) | 2005-05-23 | 2005-05-23 | Method and device for temping and / or correction of the ignition timing of a projectile |
DE502006009327T Active DE502006009327D1 (en) | 2005-05-23 | 2006-02-01 | Method and device for temping and / or correction of the ignition timing of a projectile |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE502006009327T Active DE502006009327D1 (en) | 2005-05-23 | 2006-02-01 | Method and device for temping and / or correction of the ignition timing of a projectile |
Country Status (9)
Country | Link |
---|---|
US (1) | US20070074625A1 (en) |
EP (1) | EP1726911B1 (en) |
JP (1) | JP5005954B2 (en) |
AT (1) | ATE506594T1 (en) |
CA (1) | CA2545300A1 (en) |
DE (2) | DE102005024179A1 (en) |
DK (1) | DK1726911T3 (en) |
ES (1) | ES2365039T3 (en) |
ZA (1) | ZA200604101B (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008067876A1 (en) | 2006-12-08 | 2008-06-12 | Rheinmetall Air Defence Ag | Method for measurement of the muzzle velocity of a projectile or the like |
DE102007007404A1 (en) | 2007-02-12 | 2008-08-14 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Method and device for remote release of a projectile |
WO2008098562A1 (en) | 2007-02-12 | 2008-08-21 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Method and device for defence against airborne assault ammunition |
WO2009036858A1 (en) * | 2007-09-18 | 2009-03-26 | Rheinmetall Air Defence Ag | Method and apparatus for increasing the hit accuracy in munition decomposition which in particular is time-controlled |
DE102008024574A1 (en) | 2008-05-21 | 2010-06-17 | Rheinmetall Air Defence Ag | Apparatus and method for measuring the muzzle velocity of a projectile or the like |
DE102012022894A1 (en) * | 2012-11-23 | 2014-05-28 | Gabriele Lisa Trinkel | System for identification, verification and/or authentication of projectile e.g. railgun projectile, has sensor, communication unit, processing unit and power supply or power generation unit which are arranged in housing of projectile |
RU2535313C2 (en) * | 2010-02-01 | 2014-12-10 | Рейнметалл Эйр Дифенс Аг | Programmable shell |
RU2539091C2 (en) * | 2010-02-01 | 2015-01-10 | Рейнметалл Эйр Дифенс Аг | Method and apparatus for programming projectile |
EP2989408B1 (en) | 2013-04-26 | 2021-03-17 | Rheinmetall Waffe Munition GmbH | Method for operating a weapon system |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
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SG155076A1 (en) * | 2008-02-18 | 2009-09-30 | Advanced Material Engineering | In-flight programming of trigger time of a projectile |
DE102008052074A1 (en) * | 2008-10-17 | 2010-04-22 | Rheinmetall Landsysteme Gmbh | Weapon system with a carrier vehicle and a vehicle-mounted mortar |
DE102008056108A1 (en) | 2008-11-06 | 2010-05-12 | Rheinmetall Waffe Munition Gmbh | Weapon with return and a damping braking device |
DE102008056112A1 (en) | 2008-11-06 | 2010-05-12 | Rheinmetall Waffe Munition Gmbh | mortar |
DE102009011447B9 (en) * | 2009-03-03 | 2012-08-16 | Diehl Bgt Defence Gmbh & Co. Kg | Method for igniting a warhead of a grenade and vehicle |
DE102009024508A1 (en) | 2009-06-08 | 2011-07-28 | Rheinmetall Air Defence Ag | Method for correcting the trajectory of an end-phase guided munition |
DE102010004820A1 (en) | 2010-01-15 | 2011-07-21 | Rheinmetall Air Defence Ag | Method for trajectory correction of a particular endphase steered projectile and projectile for performing the method |
US8935958B2 (en) * | 2010-11-22 | 2015-01-20 | Drs Technologies Canada, Ltd. | Muzzle velocity sensor |
DE102011018248B3 (en) * | 2011-04-19 | 2012-03-29 | Rheinmetall Air Defence Ag | Device and method for programming a projectile |
JP5979022B2 (en) * | 2012-01-27 | 2016-08-24 | ダイキン工業株式会社 | Ammo actuation system |
CN102620603A (en) * | 2012-03-31 | 2012-08-01 | 中国人民解放军济南军区72465部队 | Installation structure of initial-speed measuring coils and time setting coil of air-defense antiaircraft gun muzzle |
GB2522246B (en) * | 2014-01-20 | 2016-05-11 | Bae Systems Plc | Fuze setting apparatus |
US10746519B2 (en) * | 2016-02-16 | 2020-08-18 | Bae Systems Plc | Fuse system for projectile |
WO2017141007A1 (en) * | 2016-02-16 | 2017-08-24 | Bae Systems Plc | Activating a fuse |
EP3208569A1 (en) * | 2016-02-16 | 2017-08-23 | BAE Systems PLC | Activating a fuse |
KR101800843B1 (en) * | 2016-05-12 | 2017-12-21 | 주식회사 한국계측기기연구센터 | calibration system for muzzle velocity doppler rader and method thereof |
KR102124083B1 (en) * | 2018-12-21 | 2020-06-17 | 주식회사 한화 | Apparatus and method for controlling safety time of electronic fuse using turbine generator |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3918061A (en) * | 1973-09-25 | 1975-11-04 | Terma Elektronisk Industri As | Velocity measuring doppler radar |
US4267776A (en) | 1979-06-29 | 1981-05-19 | Motorola, Inc. | Muzzle velocity compensating apparatus and method for a remote set fuze |
DE3307785A1 (en) * | 1983-03-04 | 1984-09-06 | Deutsch-Französisches Forschungsinstitut Saint-Louis, Saint-Louis | METHOD AND DEVICE FOR SETTING A FLOOR TIMER |
DE3309147A1 (en) * | 1983-03-15 | 1984-09-20 | Rainer Dipl.-Phys. 6901 Gaiberg Berthold | Method and arrangement for correcting an ignition time |
DE3830518A1 (en) * | 1988-09-08 | 1990-03-22 | Rheinmetall Gmbh | DEVICE FOR SETTING A FLOOR TIME |
DE3835656A1 (en) * | 1988-10-20 | 1990-04-26 | Asea Brown Boveri | Method for correction of the detonation time of a projectile which is fired from a weapon barrel, and a circuit arrangement for carrying out the method |
DE3835655A1 (en) * | 1988-10-20 | 1990-04-26 | Asea Brown Boveri | Method for correction of the detonation point of a projectile |
ATE96536T1 (en) * | 1990-07-19 | 1993-11-15 | Contraves Ag | RECEIVER COIL FOR A PROGRAMMABLE FUZE. |
US5497704A (en) * | 1993-12-30 | 1996-03-12 | Alliant Techsystems Inc. | Multifunctional magnetic fuze |
CH691143A5 (en) | 1995-03-17 | 2001-04-30 | Contraves Ag | Device for measuring shell velocity at mouth of barrel of high cadence weapon has offset magnetic flux sensor coils on closed magnetic circuit perpendicular to barrel |
EP0769673B1 (en) * | 1995-09-28 | 2002-03-20 | Oerlikon Contraves Pyrotec AG | Method and device to program time fuses for projectiles |
FR2761767B1 (en) * | 1997-04-03 | 1999-05-14 | Giat Ind Sa | METHOD FOR PROGRAMMING IN FLIGHT A TRIGGERING MOMENT OF A PROJECTILE ELEMENT, FIRE CONTROL AND ROCKET IMPLEMENTING SUCH A METHOD |
DE59806709D1 (en) * | 1997-11-19 | 2003-01-30 | Contraves Ag | Projectile with programmable timer |
EP0992762B1 (en) * | 1998-10-08 | 2002-03-06 | Oerlikon Contraves Ag | Method and device for transmitting information to a programmable projectile |
ATE227839T1 (en) | 1998-10-08 | 2002-11-15 | Contraves Pyrotec Ag | METHOD FOR CORRECTING A PRE-PROGRAMMED TRIGGER OF A PROCESS IN A SPIN-STABILIZED MISSILE, DEVICE FOR IMPLEMENTING THE METHOD AND USE OF THE DEVICE |
ES2284230T3 (en) * | 1998-10-08 | 2007-11-01 | Oerlikon Contraves Ag | PROCEDURE AND DEVICE FOR CORRECTING THE TIME OF DISINTEGRATION OR THE NUMBER OF REINFORCEMENT REVOLUTIONS OF A PROGRAMMABLE PROJECTABLE STABILIZED BY ROTATION. |
DE10236157A1 (en) * | 2002-08-07 | 2004-02-26 | Junghans Feinwerktechnik Gmbh & Co. Kg | Fuse for artillery ammunition, comprises infrared interface at its cap, for recording large amounts of data in form of prediction data as initializing information for onboard satellite navigation |
ATE391893T1 (en) * | 2003-02-26 | 2008-04-15 | Rwm Schweiz Ag | METHOD FOR PROGRAMMING THE DISASSEMBLY OF PROJECTILES AND TUBE WEAPONS USING A PROGRAMMING SYSTEM |
US20050126379A1 (en) * | 2003-12-10 | 2005-06-16 | Pikus Eugene C. | RF data communications link for setting electronic fuzes |
US7352319B2 (en) * | 2005-06-10 | 2008-04-01 | Honeywell International Inc. | Methods and systems utilizing Doppler prediction to enable fusing |
-
2005
- 2005-05-23 DE DE102005024179A patent/DE102005024179A1/en not_active Withdrawn
-
2006
- 2006-02-01 AT AT06002014T patent/ATE506594T1/en active
- 2006-02-01 EP EP06002014A patent/EP1726911B1/en not_active Not-in-force
- 2006-02-01 DK DK06002014.6T patent/DK1726911T3/en active
- 2006-02-01 DE DE502006009327T patent/DE502006009327D1/en active Active
- 2006-02-01 ES ES06002014T patent/ES2365039T3/en active Active
- 2006-04-28 CA CA002545300A patent/CA2545300A1/en not_active Abandoned
- 2006-05-18 US US11/436,327 patent/US20070074625A1/en not_active Abandoned
- 2006-05-19 JP JP2006140346A patent/JP5005954B2/en not_active Expired - Fee Related
- 2006-05-22 ZA ZA200604101A patent/ZA200604101B/en unknown
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7825850B2 (en) | 2006-12-08 | 2010-11-02 | Oerlikon Contraves Ag | Method for measuring the muzzle velocity of a projectile or the like |
WO2008067876A1 (en) | 2006-12-08 | 2008-06-12 | Rheinmetall Air Defence Ag | Method for measurement of the muzzle velocity of a projectile or the like |
US8020491B2 (en) | 2007-02-12 | 2011-09-20 | Krauss-Maffei Wegmann Gmbh & Co. | Method and apparatus for defending against airborne ammunition |
WO2008098562A1 (en) | 2007-02-12 | 2008-08-21 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Method and device for defence against airborne assault ammunition |
DE102007007403A1 (en) | 2007-02-12 | 2008-08-21 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Method and device for protection against flying attack ammunition |
WO2008098561A1 (en) | 2007-02-12 | 2008-08-21 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Method and device for the remote triggering of a projectile |
DE102007007404A1 (en) | 2007-02-12 | 2008-08-14 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Method and device for remote release of a projectile |
WO2009036858A1 (en) * | 2007-09-18 | 2009-03-26 | Rheinmetall Air Defence Ag | Method and apparatus for increasing the hit accuracy in munition decomposition which in particular is time-controlled |
DE102007044732A1 (en) | 2007-09-18 | 2009-04-02 | Oerlikon Contraves Ag | Method and device for increasing the accuracy of a particular timed ammunition breakdown |
DE102008024574A1 (en) | 2008-05-21 | 2010-06-17 | Rheinmetall Air Defence Ag | Apparatus and method for measuring the muzzle velocity of a projectile or the like |
US8305071B2 (en) | 2008-05-21 | 2012-11-06 | Rheinmetall Air Defence Ag | Apparatus and method for measurement of the muzzle velocity of a projectile or the like |
RU2535313C2 (en) * | 2010-02-01 | 2014-12-10 | Рейнметалл Эйр Дифенс Аг | Programmable shell |
RU2539091C2 (en) * | 2010-02-01 | 2015-01-10 | Рейнметалл Эйр Дифенс Аг | Method and apparatus for programming projectile |
DE102012022894A1 (en) * | 2012-11-23 | 2014-05-28 | Gabriele Lisa Trinkel | System for identification, verification and/or authentication of projectile e.g. railgun projectile, has sensor, communication unit, processing unit and power supply or power generation unit which are arranged in housing of projectile |
EP2989408B1 (en) | 2013-04-26 | 2021-03-17 | Rheinmetall Waffe Munition GmbH | Method for operating a weapon system |
Also Published As
Publication number | Publication date |
---|---|
ZA200604101B (en) | 2007-02-28 |
ES2365039T3 (en) | 2011-09-21 |
JP5005954B2 (en) | 2012-08-22 |
CA2545300A1 (en) | 2006-11-23 |
DE502006009327D1 (en) | 2011-06-01 |
JP2006329616A (en) | 2006-12-07 |
EP1726911A1 (en) | 2006-11-29 |
EP1726911B1 (en) | 2011-04-20 |
DK1726911T3 (en) | 2011-08-01 |
US20070074625A1 (en) | 2007-04-05 |
ATE506594T1 (en) | 2011-05-15 |
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Legal Events
Date | Code | Title | Description |
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8127 | New person/name/address of the applicant |
Owner name: RHEINMETALL AIR DEFENCE AG, ZUERICH, CH |
|
R005 | Application deemed withdrawn due to failure to request examination |
Effective date: 20120524 |