Lockheed Martin C-130J-190 Hercules

GPTKB entity

Statements (57)
Predicate Object
gptkbp:instanceOf aircraft
gptkbp:armament various configurations
gptkbp:capacity up to 128 troops
gptkbp:crew 2 pilots
gptkbp:design enhanced situational awareness
modular design
state-of-the-art technology
advanced avionics
improved fuel efficiency
advanced navigation systems
reliable performance
low operating costs
integrated communication systems
increased payload capacity
fly-by-wire controls
high-wing
rear ramp door
high operational flexibility
pressurized cabin
modular mission systems
twin vertical stabilizers
retractable landing gear
enhanced survivability features
multi-role capability
versatile mission profile
advanced cargo handling systems
short takeoff and landing capability
reduced maintenance requirements
wing-mounted engines
four-engine turboprop
cargo ramp
combat-ready features
high-lift wing
cargo_hold
gptkbp:engineType gptkb:Rolls-Royce_AE_2100D3
gptkbp:firstFlight August 5, 1996
gptkbp:height 11.8 m
https://www.w3.org/2000/01/rdf-schema#label Lockheed Martin C-130J-190 Hercules
gptkbp:length 29.8 m
gptkbp:manufacturer gptkb:Lockheed_Martin
gptkbp:maximum_speed 366 knots
gptkbp:maxTakeoffWeight 75,000 lb
gptkbp:primaryUser gptkb:United_States_Air_Force
gptkbp:produces ongoing
gptkbp:range 2,400 nautical miles
gptkbp:role cargo transport
disaster relief
medical evacuation
search and rescue
firefighting
aerial refueling
tactical airlift
paratrooping
airdrop missions
gptkbp:service_ceiling 28,000 ft
gptkbp:variant gptkb:C-130J_Super_Hercules
gptkbp:wingspan 40.4 m