|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Northrop_T-38_Talon
|
|
gptkbp:aircraft_operated
|
low-wing
jet trainer
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:avionics
|
modernized systems
|
|
gptkbp:climb_rate
|
4,000 ft/min
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Northrop_Corporation
advanced jet trainer
|
|
gptkbp:developed_by
|
Northrop T-38
|
|
gptkbp:engine_type
|
twin-engine
|
|
gptkbp:exported_to
|
several countries
|
|
gptkbp:first_flight
|
gptkb:1959
|
|
gptkbp:fuel_capacity
|
1,200 lb
|
|
gptkbp:future_plans
|
continue service for training
|
|
gptkbp:height
|
12 ft 1 in
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Northrop T-38 C
|
|
gptkbp:introduced
|
gptkb:1972
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
47 ft 6 in
|
|
gptkbp:manufacturer
|
gptkb:Northrop_Corporation
|
|
gptkbp:material
|
aluminum
|
|
gptkbp:max_speed
|
Mach 1.0
|
|
gptkbp:max_takeoff_weight
|
5,500 lb
6 G
|
|
gptkbp:modifications
|
upgraded avionics
|
|
gptkbp:nickname
|
gptkb:Talon
|
|
gptkbp:number_built
|
more than 1,100
|
|
gptkbp:operational_history
|
used in various air forces
|
|
gptkbp:operational_range
|
1,200 mi
|
|
gptkbp:power_output
|
gptkb:General_Electric_J85
|
|
gptkbp:price
|
$2.5 million
|
|
gptkbp:primary_user
|
gptkb:aircraft
|
|
gptkbp:range
|
1,200 mi
|
|
gptkbp:retired
|
some air forces
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
30 degrees per second
|
|
gptkbp:seating_capacity
|
gptkb:Martin-Baker_Mk_10
1,500 lb
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:service_history
|
used for training and evaluation
|
|
gptkbp:speed
|
100 knots
|
|
gptkbp:status
|
in service
|
|
gptkbp:successor
|
gptkb:Northrop_T-38_Talon
|
|
gptkbp:surface
|
elevators
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:training
|
pilot training
advanced flight training
|
|
gptkbp:variant
|
gptkb:Northrop_T-38_Talon
|
|
gptkbp:wingspan
|
25 ft 3 in
|