Statements (56)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
7
|
| gptkbp:bfsParent |
gptkb:Mitsubishi_Ha-101
|
| gptkbp:aircraft_operated |
gptkb:Mitsubishi_A6_M_Zero
gptkb:Mitsubishi_G4_M |
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:compression_ratio |
6.5:1
|
| gptkbp:cooling_system |
liquid-cooled
water-cooled |
| gptkbp:displacement |
1,800 cc
|
| gptkbp:engine |
gptkb:aircraft
gptkb:12 1,000 hp limited production high reliability air-cooled advanced features for its time detailed specifications available excellent performance influenced future engine designs V-12 configuration faced production challenges used in several aircraft types incorporated innovative technologies recognized for its engineering excellence 2,500 RPM developed during World War II characteristics suitable for combat aircraft specifications published in aviation journals V-engine layout developed by Mitsubishi Heavy Industries focused on power and efficiency historically significant in aviation history limited production numbers due to war. performance compared favorably to contemporaries |
| gptkbp:engine_type |
no known variants
V-12 engine |
| gptkbp:first_flight |
gptkb:1944
|
| gptkbp:fuel_capacity |
400 kg
|
| gptkbp:fuel_type |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mitsubishi Ha-102
|
| gptkbp:impact |
significant impact on Japanese aviation
|
| gptkbp:is_tested_for |
extensively tested
|
| gptkbp:manufacturer |
gptkb:Mitsubishi
|
| gptkbp:notable_feature |
high power-to-weight ratio
|
| gptkbp:origin |
gptkb:Japan
|
| gptkbp:power_output |
1,000 hp
|
| gptkbp:production_years |
1944-1945
|
| gptkbp:propulsion |
variable-pitch propeller
|
| gptkbp:setting |
V-type
|
| gptkbp:successor |
gptkb:Mitsubishi_Ha-211
|
| gptkbp:torque |
1,200 Nm
|
| gptkbp:type |
piston engine
|
| gptkbp:used_in |
gptkb:Mitsubishi_J2_M_Raiden
|
| gptkbp:valve_configuration |
overhead valve
|
| gptkbp:weight |
400 kg
|