gptkbp:instanceOf
|
aircraft
|
gptkbp:aircraft
|
single-engine
high-wing
|
gptkbp:armament
|
machine guns
|
gptkbp:climbRate
|
6 m/s
|
gptkbp:cockpit
|
open cockpit
tandem_seating
|
gptkbp:commissioningDate
|
1938
|
gptkbp:constructionMaterial
|
metal
|
gptkbp:controls
|
elevators, ailerons, rudder
|
gptkbp:countryOfOrigin
|
gptkb:Japan
|
gptkbp:crew
|
1
|
gptkbp:design
|
gptkb:Kiyoshi_Saito
|
gptkbp:engine
|
gptkb:Nakajima_NK9A_engine
|
gptkbp:engineType
|
radial engine
|
gptkbp:firstFlight
|
1939
|
gptkbp:floors
|
conventional
|
gptkbp:fuelCapacity
|
300 L
|
gptkbp:height
|
3.0 m
|
gptkbp:historicalSignificance
|
early_Japanese_fighter_aircraft
|
https://www.w3.org/2000/01/rdf-schema#label
|
Nakajima NK9A
|
gptkbp:landingGear
|
tailwheel
|
gptkbp:length
|
8.5 m
|
gptkbp:manufacturer
|
gptkb:Nakajima_Aircraft_Company
|
gptkbp:maxSpeed
|
500 km/h
|
gptkbp:militaryRank
|
gptkb:Imperial_Japanese_Navy
|
gptkbp:notableFeature
|
good maneuverability
|
gptkbp:numberBuilt
|
50
|
gptkbp:operationalArea
|
combat and training
|
gptkbp:operationalStatus
|
frise ailerons
|
gptkbp:productionLocation
|
gptkb:Japan
|
gptkbp:productionYears
|
1939-1945
|
gptkbp:propulsion
|
two-bladed propeller
|
gptkbp:range
|
800 km
|
gptkbp:retired
|
1945
|
gptkbp:role
|
fighter aircraft
training aircraft
|
gptkbp:serviceHistory
|
gptkb:World_War_II
|
gptkbp:services
|
10,000 m
|
gptkbp:speed
|
80 km/h
|
gptkbp:steering
|
balanced rudder
|
gptkbp:successor
|
gptkb:Nakajima_Ki-43
|
gptkbp:usedBy
|
gptkb:Imperial_Japanese_Army_Air_Service
|
gptkbp:variant
|
gptkb:Nakajima_NK9A-1
|
gptkbp:weight
|
2,500 kg
|
gptkbp:wingArea
|
20 m²
|
gptkbp:wingspan
|
10.5 m
|