Statements (45)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft engine
|
| gptkbp:aircraft |
gptkb:Mitsubishi_A6M_Zero
|
| gptkbp:application |
military aviation
|
| gptkbp:compressionRatio |
6.5:1
|
| gptkbp:coolingSystem |
air-cooled
direct air cooling |
| gptkbp:cylinderCount |
14
|
| gptkbp:displacement |
1,500 cc
|
| gptkbp:engine |
horizontally opposed
influenced future designs conventional design advanced technology for its time lightweight for its class various aircraft applications |
| gptkbp:engineConfiguration |
mass production
radial developed_during_WWII |
| gptkbp:engineType |
piston engine
several variants produced notable features include high power |
| gptkbp:firstFlight |
1940
|
| gptkbp:fuelType |
aviation gasoline
|
| gptkbp:hasArea |
extensively tested
|
| https://www.w3.org/2000/01/rdf-schema#label |
Nakajima Ha-45
|
| gptkbp:is_used_in |
gptkb:Nakajima_Ki-43
|
| gptkbp:manufacturer |
gptkb:Nakajima_Aircraft_Company
|
| gptkbp:maximum_speed |
400 km/h
|
| gptkbp:notableUsers |
gptkb:Imperial_Japanese_Army_Air_Service
|
| gptkbp:operationalHistory |
significant historical impact
|
| gptkbp:origin |
gptkb:Japan
|
| gptkbp:performance |
high power-to-weight ratio
|
| gptkbp:performances |
high reliability
easy maintenance detailed specifications available excellent performance robust characteristics |
| gptkbp:powerOutput |
1,000 hp
|
| gptkbp:productionYears |
1940-1945
|
| gptkbp:propulsion |
variable-pitch propeller
|
| gptkbp:service_ceiling |
10,000 m
|
| gptkbp:setting |
air-cooled
|
| gptkbp:successor |
gptkb:Nakajima_Ha-115
|
| gptkbp:torque |
high torque output
|
| gptkbp:type |
radial engine
|
| gptkbp:weight |
400 kg
|