|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Yokosuka_P1_Y1
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:bore
|
15 cm
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:cooling_system
|
liquid-cooled
water-cooled
|
|
gptkbp:displacement
|
42 liters
|
|
gptkbp:engine
|
gptkb:aircraft
gptkb:14
gptkb:Mitsubishi_Heavy_Industries
high performance
high reliability
electric starter
developed during WWII
front-mounted
detailed specifications available.
2500 hp at 2800 rpm
V-14
|
|
gptkbp:engine_type
|
gptkb:engine
Kasei 26, Kasei 30
|
|
gptkbp:first_flight
|
1939
|
|
gptkbp:fuel_capacity
|
2.5 m
1.5 m
500 kg
|
|
gptkbp:fuel_type
|
gptkb:product
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi Kasei 25
|
|
gptkbp:ignition_system
|
magneto
high-tension
|
|
gptkbp:maintenance
|
periodic overhaul
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi
|
|
gptkbp:notable_users
|
gptkb:Imperial_Japanese_Navy
|
|
gptkbp:origin
|
gptkb:Japan
|
|
gptkbp:power_output
|
2500 hp
|
|
gptkbp:production_years
|
1939-1945
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:setting
|
V-type
|
|
gptkbp:stroke
|
15 cm
|
|
gptkbp:successor
|
Mitsubishi Kasei 26
|
|
gptkbp:torque
|
3000 Nm
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Mitsubishi_aircraft
|
|
gptkbp:valve_configuration
|
pushrod
|
|
gptkbp:weight
|
500 kg
|