Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft engine
|
| gptkbp:application |
military aviation
|
| gptkbp:compressionRatio |
6.5:1
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:cylinderCount |
14
|
| gptkbp:displacement |
41.5 L
|
| gptkbp:engine |
aircraft engine layout
|
| gptkbp:engineConfiguration |
horizontally opposed
|
| gptkbp:engineType |
piston engine
|
| gptkbp:firstFlight |
1940
|
| gptkbp:fuelType |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mitsubishi M-62
|
| gptkbp:is_used_in |
gptkb:Mitsubishi_G4M
|
| gptkbp:manufacturer |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:notableUsers |
gptkb:Imperial_Japanese_Navy
|
| gptkbp:origin |
gptkb:Japan
|
| gptkbp:powerOutput |
1,600 hp
|
| gptkbp:productionYears |
1940-1945
|
| gptkbp:propulsion |
variable-pitch propeller
|
| gptkbp:related_engine |
Mitsubishi_radial_engines
|
| gptkbp:setting |
14-cylinder
|
| gptkbp:successor |
Mitsubishi_M-63
|
| gptkbp:type |
radial engine
|
| gptkbp:weight |
450 kg
|