|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Mitsubishi_Type_13
|
|
gptkbp:aircraft_operated
|
gptkb:Mitsubishi_Ki-21
gptkb:Mitsubishi_Ki-67
gptkb:Mitsubishi_G4_M
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:cooling_system
|
liquid cooling
liquid-cooled
water-cooled
|
|
gptkbp:displacement
|
1,600 cc
|
|
gptkbp:engine
|
gptkb:16
gptkb:Mitsubishi_Heavy_Industries
gptkb:battle
high
high power-to-weight ratio
inline engine
good performance at altitude
nose-mounted
2500 RPM
V-16
149 k W
V-16 configuration
developed during 1930s.
naval bombers
|
|
gptkbp:engine_type
|
reciprocating engine
B16 M-1
|
|
gptkbp:first_flight
|
1939
|
|
gptkbp:fuel_capacity
|
0.9 m
1.8 m
200 g/k Wh
|
|
gptkbp:fuel_type
|
kerosene
carbureted
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi B16 M
|
|
gptkbp:ignition_system
|
magneto ignition
|
|
gptkbp:maintenance
|
moderate
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:operational_history
|
gptkb:World_War_II
|
|
gptkbp:origin
|
gptkb:Japan
|
|
gptkbp:power_output
|
200 hp
|
|
gptkbp:production_years
|
1939-1945
|
|
gptkbp:setting
|
V-type engine
|
|
gptkbp:successor
|
gptkb:Mitsubishi_B-26_engine
|
|
gptkbp:torque
|
400 Nm
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
Mitsubishi B-16 aircraft
|
|
gptkbp:valve_configuration
|
overhead valve
|
|
gptkbp:weight
|
400 kg
|