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gptkbp:instanceOf
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gptkb:aircraft
|
|
gptkbp:avionics
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glass cockpit
head-up displays
digital autopilot
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|
gptkbp:cabinWidth
|
3.12 m
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|
gptkbp:capacity
|
19,958 kg
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|
gptkbp:cargoHoldHeight
|
2.74 m
|
|
gptkbp:cargoHoldLength
|
12.5 m
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:crew
|
2
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|
gptkbp:cruiseSpeed
|
671 km/h
|
|
gptkbp:developedBy
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gptkb:Lockheed_C-130_Hercules
|
|
gptkbp:engine
|
gptkb:Rolls-Royce_AE_2100D3
|
|
gptkbp:engineType
|
turboprop
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|
gptkbp:exportedTo
|
over 20 countries
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|
gptkbp:firstFlight
|
5 April 1996
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gptkbp:height
|
11.9 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lockheed C-130J Hercules
|
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gptkbp:ICAOTypeDesignator
|
gptkb:C130
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|
gptkbp:introduced
|
1999
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|
gptkbp:length
|
29.3 m
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:maximumSpeed
|
671 km/h
|
|
gptkbp:maxTakeoffWeight
|
74,389 kg
|
|
gptkbp:NATOReportingName
|
gptkb:Super_Hercules
|
|
gptkbp:nickname
|
gptkb:Super_Hercules
|
|
gptkbp:notableFeature
|
improved performance over previous C-130 models
increased range and speed
reduced crew requirements
|
|
gptkbp:numberBuilt
|
over 500
|
|
gptkbp:numberOfEngines
|
4
|
|
gptkbp:primaryUser
|
gptkb:Royal_Air_Force
gptkb:United_States_Air_Force
gptkb:Indian_Air_Force
gptkb:Royal_Australian_Air_Force
|
|
gptkbp:propulsion
|
6-bladed composite
|
|
gptkbp:range
|
3,334 km
|
|
gptkbp:role
|
tactical airlift
|
|
gptkbp:serviceCeiling
|
8,615 m
|
|
gptkbp:status
|
in service
|
|
gptkbp:usedIn
|
gptkb:Iraq_War
gptkb:War_in_Afghanistan
various humanitarian missions
|
|
gptkbp:variant
|
gptkb:HC-130J
gptkb:AC-130J
gptkb:C-130J-30
gptkb:KC-130J
gptkb:MC-130J
|
|
gptkbp:wingspan
|
39.7 m
|
|
gptkbp:bfsParent
|
gptkb:RAF
gptkb:RAF_Brize_Norton
|
|
gptkbp:bfsLayer
|
5
|