Properties (50)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft engine
|
| gptkbp:aircraft |
gptkb:Mitsubishi_G4M
gptkb:Mitsubishi_Ki-21 |
| gptkbp:application |
military aviation
|
| gptkbp:bore |
120 mm
|
| gptkbp:built |
approximately 1,000
|
| gptkbp:commissioningDate |
1935
|
| gptkbp:compressionRatio |
6.5:1
|
| gptkbp:coolingSystem |
air-cooled
effective under various conditions |
| gptkbp:displacement |
1,000 cc
|
| gptkbp:drivetrain |
overhead valve
|
| gptkbp:engine |
various aircraft models
horizontally opposed influenced future designs. minimized for stability Mitsubishi_design_team |
| gptkbp:engineConfiguration |
aircraft engine
|
| gptkbp:engineType |
lightweight construction
piston engine M-33A, M-33B |
| gptkbp:firstFlight |
1936
|
| gptkbp:fuel_capacity |
efficient for long flights
|
| gptkbp:fuelType |
aviation gasoline
magneto |
| gptkbp:hasArea |
conducted_in_Japan
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mitsubishi M-33
|
| gptkbp:is_used_in |
Mitsubishi Ki-15
|
| gptkbp:manufacturer |
gptkb:Mitsubishi
|
| gptkbp:noise_level |
moderate during operation
|
| gptkbp:operational_status |
gptkb:World_War_II
|
| gptkbp:origin |
gptkb:Japan
|
| gptkbp:performances |
reliable
optimized for performance routine checks required detailed in technical manuals high during service life required after certain hours of operation |
| gptkbp:powerOutput |
100 hp
|
| gptkbp:productionYears |
1936-1940
|
| gptkbp:propulsion |
fixed-pitch
sufficient for takeoff |
| gptkbp:related_engine |
gptkb:Mitsubishi_M_series
four-stroke |
| gptkbp:setting |
9-cylinder
|
| gptkbp:stroke |
120 mm
|
| gptkbp:successor |
gptkb:Mitsubishi_M-62
|
| gptkbp:torque |
adequate for aircraft performance
|
| gptkbp:type |
radial engine
|
| gptkbp:weight |
150 kg
|