Statements (46)
Predicate | Object |
---|---|
gptkbp:instanceOf |
aircraft engine
|
gptkbp:application |
military aircraft
|
gptkbp:compressionRatio |
6.5:1
|
gptkbp:coolingSystem |
air-cooled
|
gptkbp:cylinderCount |
9 cylinders
|
gptkbp:displacement |
1,200 cubic inches
|
gptkbp:drivetrain |
pushrod
|
gptkbp:engine |
historical significance
fighter aircraft advanced technology for its time radial layout Nakajima_design |
gptkbp:engineConfiguration |
World War II era
limited production horizontally opposed |
gptkbp:engineType |
piston engine
supercharged NK9K-1 |
gptkbp:firstFlight |
1940s
|
gptkbp:fuel_capacity |
200 L/h
|
gptkbp:fuelType |
aviation gasoline
magneto |
gptkbp:hasArea |
extensive testing
military certification |
https://www.w3.org/2000/01/rdf-schema#label |
Nakajima NK9K
|
gptkbp:is_used_in |
gptkb:Nakajima_Ki-43
gptkb:Nakajima_Ki-84 |
gptkbp:manufacturer |
gptkb:Nakajima_Aircraft_Company
|
gptkbp:notableUsers |
gptkb:Imperial_Japanese_Army_Air_Service
|
gptkbp:origin |
gptkb:Japan
|
gptkbp:performances |
high performance
high reliability 1,500 hours detailed specifications available moderate maintenance performance metrics documented 2,500 RPM distinctive characteristics noted. |
gptkbp:powerOutput |
1,000 horsepower
|
gptkbp:productionYears |
1940s to 1950s
|
gptkbp:propulsion |
variable pitch
|
gptkbp:related_engine |
NK series
|
gptkbp:successor |
gptkb:Nakajima_NK9H
|
gptkbp:torque |
1,200 Nm
|
gptkbp:type |
radial engine
|
gptkbp:weight |
300 kg
|