gptkbp:instance_of
|
gptkb:fighter_aircraft
|
gptkbp:aircraft_configuration
|
low-wing
|
gptkbp:aircraft_operated
|
25 years
1956-1980
|
gptkbp:aircraft_role
|
defensive
|
gptkbp:aircraft_type
|
twin-engine
|
gptkbp:aircraft_weight_empty
|
10,000 kg
|
gptkbp:aircraft_weight_loaded
|
15,000 kg
|
gptkbp:armament
|
gptkb:20_mm_M39_cannon
AIM-4 Falcon missiles
|
gptkbp:climb_rate
|
20 m/s
|
gptkbp:cockpit
|
tandem seating
|
gptkbp:country_of_origin
|
gptkb:United_States
|
gptkbp:crew
|
gptkb:Pilot
2
radar operator
|
gptkbp:cruise_speed
|
800 km/h
|
gptkbp:design
|
gptkb:Northrop
|
gptkbp:design_date
|
1945-1950
|
gptkbp:engine
|
gptkb:General_Electric_J47
|
gptkbp:engine_type
|
turbojet
|
gptkbp:first_flight
|
gptkb:1980
1951-08-16
|
gptkbp:fuel_capacity
|
3,000 liters
|
gptkbp:height
|
4.57 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
Northrop F-89 Scorpion
|
gptkbp:introduced
|
gptkb:1956
|
gptkbp:is_targeted_at
|
gptkb:radar_system
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
15.24 m
|
gptkbp:manufacturer
|
gptkb:Northrop_Corporation
|
gptkbp:max_speed
|
1,000 km/h
|
gptkbp:max_takeoff_weight
|
15,000 kg
|
gptkbp:number_built
|
1,200
|
gptkbp:payload_capacity
|
3,000 kg
|
gptkbp:primary_user
|
gptkb:United_States_Air_Force
|
gptkbp:radar
|
gptkb:AN/_APS-4
|
gptkbp:range
|
2,500 km
|
gptkbp:retired
|
gptkb:1980
|
gptkbp:role
|
interceptor
all-weather interceptor
|
gptkbp:seating_capacity
|
gptkb:Martin-Baker_ejection_seat
|
gptkbp:service
|
gptkb:1956
|
gptkbp:service_ceiling
|
12,500 m
|
gptkbp:service_history
|
gptkb:Cold_War
|
gptkbp:stall_speed
|
200 km/h
|
gptkbp:successor
|
gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
|
gptkbp:used_by
|
gptkb:National_Guard
|
gptkbp:variant
|
gptkb:F-89_D
gptkb:F-89_J
|
gptkbp:wing_area
|
34.84 m²
|
gptkbp:wing_configuration
|
straight wing
|
gptkbp:wingspan
|
15.24 m
|
gptkbp:bfsParent
|
gptkb:Operation_Bodenplatte
gptkb:Operation_Rolling_Thunder_III
|
gptkbp:bfsLayer
|
5
|