|
gptkbp:instanceOf
|
multiple launch rocket system
|
|
gptkbp:abilities
|
firing guided rockets
firing tactical missiles
|
|
gptkbp:armament
|
aluminum alloy
12 × 227 mm rockets
2 × MGM-140 ATACMS missiles
|
|
gptkbp:category
|
gptkb:aircraft
artillery
|
|
gptkbp:chassis
|
gptkb:Bradley_Fighting_Vehicle_chassis
|
|
gptkbp:combatWeight
|
25,000 kg
|
|
gptkbp:controls
|
gptkb:Improved_Fire_Control_System_(IFCS)
|
|
gptkbp:crew
|
3
|
|
gptkbp:engine
|
gptkb:Detroit_Diesel_8V71T
|
|
gptkbp:enginePower
|
500 hp
|
|
gptkbp:enteredService
|
2005
|
|
gptkbp:fuelType
|
617 liters
|
|
gptkbp:height
|
2.59 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
M270A1 MLRS
|
|
gptkbp:introduced
|
2005
|
|
gptkbp:launcherLoaderModule
|
gptkb:Improved_Launcher_Loader_Module_(ILM)
|
|
gptkbp:length
|
6.85 m
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:maximumSpeed
|
64 km/h
|
|
gptkbp:notableFeature
|
reduced crew workload
improved accuracy
capable of firing GMLRS
faster launch procedures
|
|
gptkbp:notableRelease
|
M270 MLRS
|
|
gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:range
|
480 km
|
|
gptkbp:rangeWithATACMS
|
up to 300 km
|
|
gptkbp:rangeWithGMLRS
|
up to 70-84 km
|
|
gptkbp:suspension
|
torsion bar
|
|
gptkbp:usedBy
|
gptkb:Japanese_Ground_Self-Defense_Force
gptkb:British_Army
gptkb:French_Army
gptkb:German_Army
gptkb:United_States_Army
gptkb:Turkish_Army
gptkb:Greek_Army
gptkb:Italian_Army
gptkb:Danish_Army
gptkb:Finnish_Army
gptkb:Egyptian_Army
gptkb:South_Korean_Army
gptkb:Norwegian_Army
gptkb:Saudi_Arabian_Army
gptkb:Ukrainian_Army
gptkb:Bahraini_Army
|
|
gptkbp:weight
|
25,000 kg
|
|
gptkbp:width
|
2.97 m
|
|
gptkbp:bfsParent
|
gptkb:75th_Field_Artillery_Brigade
|
|
gptkbp:bfsLayer
|
6
|