|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
none
air superiority
military aircraft
high maneuverability
influenced future designs
low-wing configuration
prototype specifications
|
|
gptkbp:armament
|
machine guns
|
|
gptkbp:climbRate
|
15 m/s
|
|
gptkbp:cockpit
|
single-seat cockpit
|
|
gptkbp:commissioningDate
|
1944
|
|
gptkbp:constructionMaterial
|
metal construction
|
|
gptkbp:countryOfOrigin
|
gptkb:Japan
|
|
gptkbp:crew
|
1
not applicable
|
|
gptkbp:design
|
high performance
defense against bombers
Nakajima_engineers
|
|
gptkbp:engine
|
gptkb:Nakajima_NK9H_engine
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1945
limited flight testing
|
|
gptkbp:fuelCapacity
|
500 liters
|
|
gptkbp:headlights
|
conventional tail
|
|
gptkbp:historicalContext
|
gptkb:World_War_II
|
|
gptkbp:historicalSignificance
|
post-war development
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Nakajima NK9H
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
8.5 meters
|
|
gptkbp:manufacturer
|
gptkb:Nakajima_Aircraft_Company
|
|
gptkbp:maxSpeed
|
600 km/h
|
|
gptkbp:maxTakeoffWeight
|
2,500 kg
|
|
gptkbp:missions
|
manual control
|
|
gptkbp:numberBuilt
|
1
|
|
gptkbp:produces
|
not mass-produced
|
|
gptkbp:propulsion
|
two-bladed propeller
|
|
gptkbp:relatedAircraft
|
gptkb:Nakajima_Ki-84
|
|
gptkbp:role
|
interceptor
|
|
gptkbp:service_ceiling
|
10,000 meters
|
|
gptkbp:services
|
10,000 meters
|
|
gptkbp:status
|
prototype
|
|
gptkbp:succeededBy
|
30 degrees/second
|
|
gptkbp:supportRole
|
none
|
|
gptkbp:takeoffDistance
|
400 meters
300 meters
120 km/h
|
|
gptkbp:team
|
Nakajima_design_team
|
|
gptkbp:type
|
fighter aircraft
|
|
gptkbp:weight
|
1,800 kg
|
|
gptkbp:wingArea
|
20 m²
|
|
gptkbp:wingspan
|
10.5 meters
|