EP2767795A3 - Method for operating a stationary missile - Google Patents

Method for operating a stationary missile Download PDF

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Publication number
EP2767795A3
EP2767795A3 EP14000284.1A EP14000284A EP2767795A3 EP 2767795 A3 EP2767795 A3 EP 2767795A3 EP 14000284 A EP14000284 A EP 14000284A EP 2767795 A3 EP2767795 A3 EP 2767795A3
Authority
EP
European Patent Office
Prior art keywords
control unit
operating
missile
stationary
stationary missile
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Withdrawn
Application number
EP14000284.1A
Other languages
German (de)
French (fr)
Other versions
EP2767795A2 (en
Inventor
Stephan Truckenbrodt
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Diehl Defence GmbH and Co KG
Original Assignee
Diehl Defence GmbH and Co KG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Diehl Defence GmbH and Co KG filed Critical Diehl Defence GmbH and Co KG
Publication of EP2767795A2 publication Critical patent/EP2767795A2/en
Publication of EP2767795A3 publication Critical patent/EP2767795A3/en
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B35/00—Testing or checking of ammunition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F41F3/06—Rocket or torpedo launchers for rockets from aircraft
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/01—Arrangements thereon for guidance or control
    • 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
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F41F3/055—Umbilical connecting means

Abstract

Die Erfindung geht aus von einem Verfahren zum Betrieb eines ruhenden Flugkörpers (4), bei dem ein Bediengerät (28) signaltechnisch mit einer im ruhenden Flugkörper (4) angeordneten Steuereinheit (14), die zur Steuerung von Betriebsfunktionen vorbereitet ist, verbunden wird und Daten zwischen Bediengerät (28) und Steuereinheit (14) ausgetauscht werden.The invention is based on a method for operating a stationary missile (4), in which an operating device (28) is signal-connected to a control unit (14) arranged in the stationary missile (4), which is prepared for controlling operating functions, and data between control unit (28) and control unit (14) are exchanged.

Zur Erleichterung des Betriebs wird vorgeschlagen, dass die Steuereinheit (14) über eine Leitung (24) mit einer Sende- und Empfangseinheit (26a, 26b, 26c) verbunden ist und die Daten zwischen Steuereinheit (14) und dem Bediengerät (28) von der Sendeund Empfangseinheit (26a, 26b, 26c) drahtlos übertragen werden.

Figure imgaf001
To facilitate the operation, it is proposed that the control unit (14) via a line (24) with a transmitting and receiving unit (26a, 26b, 26c) is connected and the data between the control unit (14) and the control unit (28) of the Transmitting and receiving unit (26a, 26b, 26c) are transmitted wirelessly.
Figure imgaf001
EP14000284.1A 2013-02-16 2014-01-28 Method for operating a stationary missile Withdrawn EP2767795A3 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102013002717.9A DE102013002717A1 (en) 2013-02-16 2013-02-16 Method for operating a stationary missile

Publications (2)

Publication Number Publication Date
EP2767795A2 EP2767795A2 (en) 2014-08-20
EP2767795A3 true EP2767795A3 (en) 2017-07-26

Family

ID=50031127

Family Applications (1)

Application Number Title Priority Date Filing Date
EP14000284.1A Withdrawn EP2767795A3 (en) 2013-02-16 2014-01-28 Method for operating a stationary missile

Country Status (2)

Country Link
EP (1) EP2767795A3 (en)
DE (1) DE102013002717A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014017653A1 (en) * 2014-12-01 2016-06-02 Mbda Deutschland Gmbh Transport and storage container for a missile
CN106855380B (en) * 2015-12-08 2018-10-16 上海机电工程研究所 A kind of method of guided missile test set power switching
DE102016000121A1 (en) * 2016-01-08 2017-07-13 Mbda Deutschland Gmbh Multifunctional testing device for arming
CN109341440B (en) * 2018-11-14 2023-10-20 中国空空导弹研究院 Telemetry device conformal with missile cable fairing
CN208775022U (en) * 2018-12-03 2019-04-23 中国航空工业集团公司沈阳飞机设计研究所 External aircraft mounted control system
CN111397865B (en) * 2019-12-10 2021-11-23 北京航空航天大学 Performance test platform for piston buffer device of launching tube

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008112012A2 (en) * 2006-10-04 2008-09-18 Raytheon Company Supercapacitor power supply
US8009060B2 (en) * 2001-09-26 2011-08-30 Lockheed Martin Corporation Remote monitoring of munition assets
EP2390615A1 (en) * 2010-05-27 2011-11-30 LFK-Lenkflugkörpersysteme GmbH Method for accessing measurement and/or status data from a data storage unit of a sharp unmanned aerial vehicle and device for performing the method
US8256338B1 (en) * 2010-01-06 2012-09-04 The United States Of America As Represented By The Secretary Of The Navy Weapon and weapon station system and method for loading, testing, targeting, and launching a weapon

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8009060B2 (en) * 2001-09-26 2011-08-30 Lockheed Martin Corporation Remote monitoring of munition assets
WO2008112012A2 (en) * 2006-10-04 2008-09-18 Raytheon Company Supercapacitor power supply
US8256338B1 (en) * 2010-01-06 2012-09-04 The United States Of America As Represented By The Secretary Of The Navy Weapon and weapon station system and method for loading, testing, targeting, and launching a weapon
EP2390615A1 (en) * 2010-05-27 2011-11-30 LFK-Lenkflugkörpersysteme GmbH Method for accessing measurement and/or status data from a data storage unit of a sharp unmanned aerial vehicle and device for performing the method

Also Published As

Publication number Publication date
EP2767795A2 (en) 2014-08-20
DE102013002717A1 (en) 2014-08-21

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