|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Northrop_T-38_Talon
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
gptkb:Boeing_T-7_Red_Hawk
gptkb:Lockheed_Martin_F-16_Fighting_Falcon
gptkb:Northrop_F-5
low-wing
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:avionics
|
modernized avionics
|
|
gptkbp:climb_rate
|
4,000 ft/min
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Northrop_T-38_Talon
Northrop engineers
|
|
gptkbp:engine_type
|
twin-engine
|
|
gptkbp:first_flight
|
gptkb:1959
|
|
gptkbp:fuel_capacity
|
1,200 lb
|
|
gptkbp:height
|
12 ft 1 in
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Northrop T-38 C Talon II
|
|
gptkbp:influenced_by
|
gptkb:Northrop_F-5_Freedom_Fighter
|
|
gptkbp:introduced
|
gptkb:1961
|
|
gptkbp:landing_gear
|
tricycle landing gear
|
|
gptkbp:length
|
47 ft 6 in
|
|
gptkbp:manufacturer
|
gptkb:Northrop_Corporation
|
|
gptkbp:max_speed
|
Mach 1.0
|
|
gptkbp:max_takeoff_weight
|
12,000 lb
|
|
gptkbp:nickname
|
gptkb:Talon
|
|
gptkbp:notable_features
|
twin-engine design
|
|
gptkbp:number_built
|
over 1,100
|
|
gptkbp:operational_area
|
training and evaluation
|
|
gptkbp:operational_history
|
used by several air forces
|
|
gptkbp:power_output
|
gptkb:General_Electric_J85
|
|
gptkbp:price
|
$2.5 million
|
|
gptkbp:primary_user
|
gptkb:aircraft
|
|
gptkbp:range
|
1,200 miles
|
|
gptkbp:retirement_year
|
still in service
|
|
gptkbp:role
|
advanced jet trainer
fighter lead-in trainer
|
|
gptkbp:roll_rate
|
30 degrees per second
|
|
gptkbp:seating_capacity
|
gptkb:Martin-Baker_Mk._16
3,000 lb
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:services
|
gptkb:1961
|
|
gptkbp:speed
|
90 knots
|
|
gptkbp:successor
|
Northrop T-38 D
|
|
gptkbp:training
|
pilot training
|
|
gptkbp:used_in
|
air force training programs
|
|
gptkbp:variant
|
gptkb:T-38_A
gptkb:T-38_B
gptkb:T-38_C
|
|
gptkbp:wing_area
|
300 sq ft
|
|
gptkbp:wingspan
|
25 ft 3 in
|