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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
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|
gptkbp:bfsParent
|
gptkb:General_Electric_J47
|
|
gptkbp:aircraft_operated
|
twin-engine
high maneuverability
low-wing
subsonic
fly-by-wire system
advanced trainer
basic and advanced training
fourth generation
training and evaluation
jet pilot training
training future naval aviators
Hawk family
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:avionics
|
modern avionics suite
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:combat_radius
|
500 nautical miles
|
|
gptkbp:commander
|
carrier-based training
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:aircraft
|
|
gptkbp:engine
|
gptkb:Rolls-Royce_F405-RR-401
|
|
gptkbp:features
|
high-mounted wings
|
|
gptkbp:first_flight
|
gptkb:1988
|
|
gptkbp:fuel_capacity
|
2,500 liters
|
|
gptkbp:height
|
4.57 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
T-45 A Goshawk
|
|
gptkbp:introduced
|
gptkb:1991
|
|
gptkbp:landing_gear
|
tricycle landing gear
|
|
gptkbp:length
|
12.19 m
|
|
gptkbp:manufacturer
|
gptkb:Mc_Donnell_Douglas
|
|
gptkbp:material
|
composite materials
|
|
gptkbp:max_speed
|
1,050 km/h
|
|
gptkbp:max_takeoff_weight
|
5,400 kg
|
|
gptkbp:number_built
|
over 200
|
|
gptkbp:operational_area
|
gptkb:1991
naval aviation schools
|
|
gptkbp:operational_range
|
1,200 nautical miles
|
|
gptkbp:operational_status
|
in service
|
|
gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:primary_user
|
gptkb:battle
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
30 degrees per second
|
|
gptkbp:seating_capacity
|
gptkb:Martin-Baker_Mk_16
|
|
gptkbp:service_ceiling
|
15,240 m
|
|
gptkbp:service_history
|
used in naval aviation training
|
|
gptkbp:speed
|
800 km/h
110 knots
|
|
gptkbp:successor
|
gptkb:T-6_Texan_II
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:training
|
jet training
integrated training system
|
|
gptkbp:variant
|
gptkb:T-45_C_Goshawk
|
|
gptkbp:wingspan
|
9.14 m
|