EP2618099A3 - Test and test device for a missile launching device and method for testing and/or testing the functionality of a missile launching device - Google Patents

Test and test device for a missile launching device and method for testing and/or testing the functionality of a missile launching device Download PDF

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Publication number
EP2618099A3
EP2618099A3 EP13000176.1A EP13000176A EP2618099A3 EP 2618099 A3 EP2618099 A3 EP 2618099A3 EP 13000176 A EP13000176 A EP 13000176A EP 2618099 A3 EP2618099 A3 EP 2618099A3
Authority
EP
European Patent Office
Prior art keywords
test
missile
testing
computer
missile launching
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
Application number
EP13000176.1A
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German (de)
French (fr)
Other versions
EP2618099A2 (en
EP2618099B1 (en
EP2618099B8 (en
Inventor
Karl Fischer
Michael Grabmeier
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.)
MBDA Deutschland GmbH
Original Assignee
MBDA Deutschland GmbH
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Publication date
Application filed by MBDA Deutschland GmbH filed Critical MBDA Deutschland GmbH
Publication of EP2618099A2 publication Critical patent/EP2618099A2/en
Publication of EP2618099A3 publication Critical patent/EP2618099A3/en
Publication of EP2618099B1 publication Critical patent/EP2618099B1/en
Application granted granted Critical
Publication of EP2618099B8 publication Critical patent/EP2618099B8/en
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Anticipated expiration legal-status Critical

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B35/00Testing or checking of ammunition
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A31/00Testing arrangements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/001Devices or systems for testing or checking
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/006Guided missiles training or simulation devices

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Testing Of Engines (AREA)

Abstract

Eine Prüf- und Testvorrichtung für ein Flugkörperstartgerät (1), das zumindest eine Startvorrichtung (10; 12) für zumindest einen Flugkörper (10A, 10B, 10C, 10D; 12A, 12B, 12C, 12D) und einen dieser zugeordneten und von einer Waffensystemzentrale (3) steuerbaren Waffensteuerungscomputer (14) aufweist, auf dem ein Steuerungsprogramm für den Start des Flugkörpers ablaufbar installiert ist, und wobei die Startvorrichtung (10; 12) mit zumindest einer elektrischen Anschlusseinrichtung (100; 120) versehen ist, die zur Datenübertragung mit dem Waffensteuerungscomputer verbunden ist und die dem zumindest einen Flugkörper (10A, 10B, 10C, 10D; 12A, 12B, 12C, 12D) zugeordnet und mit diesem verbindbar ist und Kommunikationsanschüsse (101, 102, 103, 104; 121, 122, 123, 124) zur unidirektionalen und/oder bidirektionalen Datenübertragung zum Flugkörper (10A, 10B, 10C, 10D; 12A, 12B, 12C, 12D) aufweist, zeichnet sich dadurch aus, dass die Prüf- und Testvorrichtung einen Prüf- und Testcomputer (40) sowie zumindest eine Flugkörpersimulationseinheit (42) aufweist; dass der Prüf- und Testcomputer (40) als Simulator für zumindest einen Teil des Funktionen der Waffensystemzentrale (3) ausgebildet ist; dass der Prüf- und Testcomputer (40) zur Datenübertragung mit dem Waffensteuerungscomputer (14) verbindbar ist; und dass die Flugkörpersimulationseinheit (42) einerseits mit dem Prüf- und Testcomputer (40) zum Datenaustausch verbunden ist und andererseits mit den Kommunikationsanschlüssen der elektrischen Anschlusseinrichtung (100; 120) verbindbar ist.

Figure imgaf001
A test and test device for a missile launch device (1) comprising at least one launch device (10; 12) for at least one missile (10A, 10B, 10C, 10D; 12A, 12B, 12C, 12D) and one associated therewith and from a weapons system center (3) controllable weapon control computer (14) on which a missile launch control program is installed, and wherein the starting device (10; 12) is provided with at least one electrical connection device (100; Weapon control computer is connected and which is the at least one missile (10A, 10B, 10C, 10D, 12A, 12B, 12C, 12D) associated with and connectable to this and Kommunikationsanschüsse (101, 102, 103, 104, 121, 122, 123, 124 ) for unidirectional and / or bidirectional data transmission to the missile (10A, 10B, 10C, 10D, 12A, 12B, 12C, 12D) is characterized in that the test and test device comprises a test and test co mputer (40) and at least one missile simulation unit (42); that the test and test computer (40) is designed as a simulator for at least part of the functions of the weapon system center (3); that the test and test computer (40) for data transmission with the weapon control computer (14) is connectable; and that the missile simulation unit (42) on the one hand is connected to the test and test computer (40) for data exchange and on the other hand is connectable to the communication ports of the electrical connection device (100; 120).
Figure imgaf001

EP13000176.1A 2012-01-17 2013-01-14 Test and test device for a missile launching device and method for testing and/or testing the functionality of a missile launching device Active EP2618099B8 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102012000671.3A DE102012000671B4 (en) 2012-01-17 2012-01-17 A missile launch tester and tester and method for testing and / or testing the health of a missile launcher

Publications (4)

Publication Number Publication Date
EP2618099A2 EP2618099A2 (en) 2013-07-24
EP2618099A3 true EP2618099A3 (en) 2015-08-12
EP2618099B1 EP2618099B1 (en) 2017-06-07
EP2618099B8 EP2618099B8 (en) 2017-08-09

Family

ID=47603207

Family Applications (1)

Application Number Title Priority Date Filing Date
EP13000176.1A Active EP2618099B8 (en) 2012-01-17 2013-01-14 Test and test device for a missile launching device and method for testing and/or testing the functionality of a missile launching device

Country Status (2)

Country Link
EP (1) EP2618099B8 (en)
DE (1) DE102012000671B4 (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102013014570B4 (en) * 2013-09-02 2018-06-14 Mbda Deutschland Gmbh A method for switching on a fuel pump of a flying missile
CN104503259A (en) * 2014-11-27 2015-04-08 北京电子工程总体研究所 Universal programmable aircraft simulator system for launch control system
DE102015002563B3 (en) * 2015-02-27 2016-02-11 Mbda Deutschland Gmbh Missile launcher
DE202015004074U1 (en) 2015-02-27 2016-05-31 Mbda Deutschland Gmbh Missile launcher
DE102015006799B4 (en) * 2015-05-27 2022-11-17 Mbda Deutschland Gmbh Test facility for a missile launcher
CN105403110A (en) * 2015-12-15 2016-03-16 平顶山宇恒高科电气自动化有限公司 Exploder tester achieving self-correction of detection precision
DE102016000121A1 (en) 2016-01-08 2017-07-13 Mbda Deutschland Gmbh Multifunctional testing device for arming
US10156426B2 (en) 2016-06-21 2018-12-18 The United States Of America, As Represented By The Secretary Of The Navy Apparatus and methods for parallel testing of devices
DE102016008413A1 (en) 2016-07-13 2018-01-18 Mbda Deutschland Gmbh Multifunction control and display system
CN108761155A (en) * 2018-06-05 2018-11-06 北京电子工程总体研究所 A kind of configurable power plant simulation system
CN112344810B (en) * 2020-09-11 2022-12-13 中国运载火箭技术研究院 Missile weapon test equipment
CN112749480B (en) * 2020-12-21 2024-04-30 北京航天飞腾装备技术有限责任公司 Method for testing combination of bomb simulator and carrier
DE202021104039U1 (en) 2021-07-28 2022-11-03 Spherea Gmbh Test device for an aircraft self-protection system

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0579143A1 (en) * 1992-07-13 1994-01-19 Hughes Aircraft Company Method and apparatus for missile interface testing
US5624264A (en) * 1995-09-29 1997-04-29 The United States Of America As Represented By The Secretary Of The Navy Missile launch simulator
US20060288194A1 (en) * 2005-06-17 2006-12-21 Lewis Innovative Technologies Real-time processor

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0309133A2 (en) * 1987-09-11 1989-03-29 British Aerospace Public Limited Company Digital weapon simulator
US7228261B2 (en) * 2003-08-13 2007-06-05 The Boeing Company Methods and apparatus for testing and diagnosis of weapon control systems
US6941850B1 (en) * 2004-01-09 2005-09-13 Raytheon Company Self-contained airborne smart weapon umbilical control cable
DE102005058546A1 (en) * 2005-12-08 2007-06-14 Lfk-Lenkflugkörpersysteme Gmbh A weapons station testing unit and method of testing the operational readiness of a weapon station of an aircraft
DE102009040304B4 (en) * 2009-09-05 2012-10-04 Lfk-Lenkflugkörpersysteme Gmbh Device for controlling functional tests and / or service procedures for aircraft-unmanned aerial vehicles

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0579143A1 (en) * 1992-07-13 1994-01-19 Hughes Aircraft Company Method and apparatus for missile interface testing
US5624264A (en) * 1995-09-29 1997-04-29 The United States Of America As Represented By The Secretary Of The Navy Missile launch simulator
US20060288194A1 (en) * 2005-06-17 2006-12-21 Lewis Innovative Technologies Real-time processor

Also Published As

Publication number Publication date
EP2618099A2 (en) 2013-07-24
DE102012000671A1 (en) 2013-07-18
DE102012000671B4 (en) 2014-07-17
EP2618099B1 (en) 2017-06-07
EP2618099B8 (en) 2017-08-09

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