Statements (41)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft engine
|
| gptkbp:application |
military aircraft
|
| gptkbp:compressionRatio |
6.5:1
|
| gptkbp:coolingSystem |
air-cooled
air-cooled radial |
| gptkbp:cylinderCount |
9 cylinders
|
| gptkbp:displacement |
1,500 cubic inches
|
| gptkbp:drivetrain |
18
pushrod actuated |
| gptkbp:engine |
fighter aircraft
radial layout influenced post-war designs Nakajima_design |
| gptkbp:engineConfiguration |
limited production
horizontally opposed |
| gptkbp:engineType |
piston engine
NK9H-1,_NK9H-2 |
| gptkbp:firstFlight |
1941
|
| gptkbp:fuelType |
aviation gasoline
carbureted magneto ignition |
| gptkbp:hasArea |
extensively tested
|
| https://www.w3.org/2000/01/rdf-schema#label |
Nakajima NK9H engine
|
| gptkbp:is_used_in |
gptkb:Nakajima_Ki-43_Hayabusa
gptkb:Nakajima_Ki-84_Hayate |
| gptkbp:manufacturer |
gptkb:Nakajima_Aircraft_Company
|
| gptkbp:operationalHistory |
used_in_WWII_aircraft
|
| gptkbp:origin |
gptkb:Japan
|
| gptkbp:performances |
high performance
high reliability 2,400 RPM moderate maintenance detailed specifications available. powerful and compact |
| gptkbp:powerOutput |
1,000 horsepower
|
| gptkbp:productionYears |
1941-1945
|
| gptkbp:propulsion |
variable pitch
|
| gptkbp:related_engine |
NK series
|
| gptkbp:successor |
gptkb:Nakajima_NK9K
|
| gptkbp:type |
radial engine
|
| gptkbp:weight |
400 pounds
|