|
gptkbp:instance_of
|
gptkb:trainer_aircraft
|
|
gptkbp:aircraft_configuration
|
low-wing
|
|
gptkbp:aircraft_role
|
gptkb:training
|
|
gptkbp:aircraft_type
|
gptkb:military_aircraft
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:avionics
|
analog instruments
modernized in T-38 C
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:crew
|
2
|
|
gptkbp:cruise_speed
|
800 km/h
|
|
gptkbp:design
|
gptkb:Northrop
low-wing
advanced jet trainer
|
|
gptkbp:design_feature
|
dual controls
|
|
gptkbp:design_features
|
swept wings
high thrust-to-weight ratio
twin-engine configuration
low-wing design
|
|
gptkbp:engine
|
gptkb:General_Electric_J85
|
|
gptkbp:engine_type
|
twin-engine
|
|
gptkbp:first_flight
|
gptkb:1959
1959-04-10
still in use
April 10, 1959
|
|
gptkbp:fuel_capacity
|
1,200 liters
|
|
gptkbp:has_limitations
|
+6/-3 g
|
|
gptkbp:height
|
3.5 m
3.81 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
T-38 Talon
|
|
gptkbp:introduced
|
gptkb:1961
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
12.3 m
12.74 m
|
|
gptkbp:manufacturer
|
gptkb:Northrop
gptkb:Northrop_Corporation
|
|
gptkbp:max_speed
|
1,050 km/h
|
|
gptkbp:max_takeoff_weight
|
4,500 kg
5,400 kg
|
|
gptkbp:military_lessons
|
used for advanced training
for fighter pilots
|
|
gptkbp:nickname
|
gptkb:Talon
|
|
gptkbp:notable_pilots
|
gptkb:John_Glenn
gptkb:Neil_Armstrong
gptkb:Chuck_Yeager
|
|
gptkbp:notable_users
|
gptkb:Egyptian_Air_Force
gptkb:Philippine_Air_Force
gptkb:Singapore_Air_Force
gptkb:Test_Pilot_School
gptkb:Air_Force_Academy
gptkb:National_Guard
gptkb:United_States_Navy
gptkb:Turkish_Air_Force
gptkb:United_States_Marine_Corps
gptkb:Republic_of_Korea_Air_Force
gptkb:Taiwan_Air_Force
gptkb:NASA
gptkb:Saudi_Air_Force
International training partners
|
|
gptkbp:number_built
|
over 1,000
1,100
|
|
gptkbp:operational_history
|
used in various conflicts
used in training for astronauts
|
|
gptkbp:operational_range
|
1,200 km
|
|
gptkbp:operational_use
|
gptkb:1961
|
|
gptkbp:power_source
|
gptkb:General_Electric_J85
|
|
gptkbp:primary_function
|
pilot training
|
|
gptkbp:primary_role
|
pilot training
|
|
gptkbp:primary_user
|
gptkb:United_States_Air_Force
|
|
gptkbp:propulsion
|
2,900 lbf
|
|
gptkbp:range
|
2,000 km
|
|
gptkbp:retired
|
in service
still in service
|
|
gptkbp:retirement
|
still in service
|
|
gptkbp:role
|
advanced jet trainer
jet trainer
|
|
gptkbp:roll_rate
|
30°/s
|
|
gptkbp:seating_capacity
|
gptkb:Martin-Baker_Mk._10
|
|
gptkbp:service
|
1961-present
|
|
gptkbp:service_ceiling
|
12,500 m
13,700 m
|
|
gptkbp:service_entry
|
gptkb:1961
|
|
gptkbp:stall_speed
|
110 km/h
|
|
gptkbp:status
|
in service
|
|
gptkbp:successor
|
gptkb:T-7_Red_Hawk
gptkb:T-6_Texan_II
|
|
gptkbp:training
|
fighter pilot training
|
|
gptkbp:used_by
|
gptkb:United_States_Air_Force
gptkb:United_States_Navy
gptkb:United_States_Marine_Corps
gptkb:NASA
|
|
gptkbp:variant
|
gptkb:T-38_M
gptkb:T-38_A
gptkb:T-38_B
gptkb:T-38_C
|
|
gptkbp:wing_area
|
24.5 m²
|
|
gptkbp:wing_configuration
|
straight wing
|
|
gptkbp:wingspan
|
9.1 m
9.45 m
|
|
gptkbp:bfsParent
|
gptkb:United_States_Air_Force
|
|
gptkbp:bfsLayer
|
3
|