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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Boeing_T-45_Goshawk
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:Boeing_T-7_Red_Hawk
gptkb:Mc_Donnell_Douglas_F/_A-18_Hornet
gptkb:Mc_Donnell_Douglas_A-4_Skyhawk
low-wing monoplane
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|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:avionics
|
modern avionics suite
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:country
|
gptkb:aircraft
gptkb:Royal_Saudi_Air_Force
gptkb:battle
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Mc_Donnell_Douglas
Mc Donnell Douglas engineers
|
|
gptkbp:developer
|
gptkb:Navy's_Joint_Primary_Aircraft_Training_System
|
|
gptkbp:engine
|
gptkb:Rolls-Royce_Turbomeca_Adour
|
|
gptkbp:first_flight
|
gptkb:1988
|
|
gptkbp:fuel_capacity
|
1,800 liters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mc Donnell Douglas T-45 family
|
|
gptkbp:introduced
|
gptkb:1991
|
|
gptkbp:is_used_by
|
gptkb:battle
|
|
gptkbp:landing_gear
|
tricycle landing gear
|
|
gptkbp:length
|
12.5 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:operational_history
|
used in training for naval aviators
|
|
gptkbp:operational_range
|
1,500 km
|
|
gptkbp:primary_user
|
gptkb:battle
|
|
gptkbp:produced_by
|
over 200 units
|
|
gptkbp:role
|
gptkb:aircraft
advanced jet trainer
|
|
gptkbp:seating_capacity
|
gptkb:Martin-Baker_Mk_16
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:squadrons
|
VT-21
|
|
gptkbp:status
|
in service
|
|
gptkbp:successor
|
gptkb:T-6_Texan_II
|
|
gptkbp:training
|
naval aviators
carrier-based operations
|
|
gptkbp:type
|
jet trainer
|
|
gptkbp:variant
|
gptkb:T-45_C
gptkb:T-45_A
|
|
gptkbp:wingspan
|
9.3 m
|