Statements (39)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft engine
|
| gptkbp:application |
military aircraft
|
| gptkbp:compressionRatio |
6.5:1
|
| gptkbp:coolingSystem |
air-cooled
air-cooled design |
| gptkbp:cylinderCount |
9 cylinders
|
| gptkbp:displacement |
23 liters
|
| gptkbp:drivetrain |
overhead valves
|
| gptkbp:engine |
radial layout
influenced future aircraft engine designs incorporated advanced technologies for its time designed for bombers primarily_used_in_Japanese_military_aircraft. |
| gptkbp:engineConfiguration |
horizontally opposed
produced in large numbers |
| gptkbp:engineType |
Kasei_22,_Kasei_26
|
| gptkbp:firstFlight |
1940
|
| gptkbp:fuelType |
aviation gasoline
carburetor magneto ignition |
| gptkbp:hasArea |
extensively tested before production
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mitsubishi Kasei 23 engine
|
| gptkbp:is_used_in |
gptkb:Mitsubishi_G4M
|
| gptkbp:manufacturer |
gptkb:Mitsubishi
|
| gptkbp:maximum_speed |
maximum RPM of 2800
|
| gptkbp:operationalHistory |
gptkb:World_War_II
|
| gptkbp:performances |
high reliability
high power-to-weight ratio detailed specifications available moderate maintenance requirements notable for its power and efficiency |
| gptkbp:powerOutput |
1000 hp
|
| gptkbp:productionYears |
1940-1945
|
| gptkbp:propulsion |
variable-pitch propeller
|
| gptkbp:related_engine |
Kasei_family
|
| gptkbp:successor |
gptkb:Mitsubishi_Kasei_26_engine
|
| gptkbp:torque |
high torque output
|
| gptkbp:type |
radial engine
|
| gptkbp:weight |
400 kg
|