Properties (46)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft engine
|
| gptkbp:application |
military aircraft
|
| gptkbp:bore |
15 cm
|
| gptkbp:compressionRatio |
6.5:1
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:cylinderCount |
9 cylinders
|
| gptkbp:displacement |
1,500 cc
|
| gptkbp:drivetrain |
overhead valves
|
| gptkbp:engine |
0.9 m
1.5 m 1.2 m horizontally opposed advanced for its time. fighter aircraft, bomber aircraft influenced post-war aircraft engine designs |
| gptkbp:engineConfiguration |
radial
produced in large numbers during the war radial engine with 9 cylinders |
| gptkbp:enginePower |
1,000 hp at 2,400 rpm
|
| gptkbp:engineType |
piston engine
reliable performance under various conditions NK9B,_NK9C |
| gptkbp:firstFlight |
1940
|
| gptkbp:fuelType |
spark ignition
aviation gasoline carburetor |
| gptkbp:hasArea |
extensively tested before production
|
| https://www.w3.org/2000/01/rdf-schema#label |
Nakajima NK9A engine
|
| gptkbp:is_used_in |
gptkb:Nakajima_Ki-43
gptkb:Nakajima_Ki-84 |
| gptkbp:manufacturer |
gptkb:Nakajima_Aircraft_Company
|
| gptkbp:operationalHistory |
used_extensively_in_WWII
|
| gptkbp:origin |
gptkb:Japan
|
| gptkbp:performances |
high power-to-weight ratio
moderate maintenance requirements high reliability in combat designed for high altitude performance |
| gptkbp:powerOutput |
1,000 hp
|
| gptkbp:productionYears |
1940-1945
|
| gptkbp:propulsion |
variable-pitch propeller
|
| gptkbp:stroke |
4-stroke
15 cm |
| gptkbp:successor |
gptkb:Nakajima_NK9B_engine
|
| gptkbp:torque |
1,200 Nm
|
| gptkbp:type |
radial engine
|
| gptkbp:weight |
200 kg
|