|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
single-engine
|
|
gptkbp:aircraft_era
|
late 1940s
|
|
gptkbp:aircraft_operated
|
gptkb:military_aircraft
3,000 kg
|
|
gptkbp:aircraft_role
|
defense
|
|
gptkbp:armament
|
machine guns
|
|
gptkbp:climb_rate
|
10 m/s
|
|
gptkbp:cockpit
|
forward
enclosed
|
|
gptkbp:control_surfaces
|
elevators
ailerons
rudder
|
|
gptkbp:country_of_origin
|
gptkb:Japan
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:design
|
gptkb:Kiyoshi_Saito
|
|
gptkbp:design_date
|
gptkb:1944
|
|
gptkbp:design_features
|
streamlined fuselage
|
|
gptkbp:design_philosophy
|
performance-oriented
|
|
gptkbp:development
|
gptkb:World_War_II
|
|
gptkbp:engine
|
Nakajima NK9 H engine
|
|
gptkbp:first_flight
|
1945
|
|
gptkbp:fuel_capacity
|
300 liters
|
|
gptkbp:historical_significance
|
Japanese aviation history
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Nakajima NK9 H
|
|
gptkbp:influences
|
American fighters
|
|
gptkbp:landing_distance
|
400 m
120 km/h
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.5 m
|
|
gptkbp:manufacturer
|
gptkb:Nakajima_Aircraft_Company
|
|
gptkbp:max_speed
|
600 km/h
|
|
gptkbp:max_takeoff_weight
|
3,000 kg
|
|
gptkbp:number_built
|
gptkb:1
|
|
gptkbp:production_years
|
1945
|
|
gptkbp:propulsion
|
piston engine
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:related_aircraft
|
gptkb:Nakajima_Ki-84_Hayate
|
|
gptkbp:role
|
interceptor
|
|
gptkbp:service_ceiling
|
10,000 m
|
|
gptkbp:service_history
|
gptkb:none
|
|
gptkbp:status
|
gptkb:prototype
|
|
gptkbp:takeoff_distance
|
300 m
|
|
gptkbp:type
|
gptkb:fighter_aircraft
|
|
gptkbp:weight
|
2,200 kg
|
|
gptkbp:wing_area
|
20 m²
|
|
gptkbp:wing_configuration
|
low-wing
|
|
gptkbp:wingspan
|
10.5 m
|
|
gptkbp:bfsParent
|
gptkb:Nakajima_NK9_A
|
|
gptkbp:bfsLayer
|
6
|