|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Kawasaki_Ki-61
gptkb:Nakajima_Ki-43
gptkb:Mitsubishi_A6_M_Zero
gptkb:Mitsubishi_G4_M
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:configuration
|
9-cylinder
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:displacement
|
1,800 cubic inches
|
|
gptkbp:engine_configuration
|
radial
horizontally opposed
9-cylinder radial
|
|
gptkbp:engine_displacement
|
29.5 L
|
|
gptkbp:engine_power
|
1,000 hp
2,400 RPM
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
1941
|
|
gptkbp:fuel_capacity
|
1,000 mm
400 kg
1,200 mm
|
|
gptkbp:fuel_type
|
aviation gasoline
carbureted
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Nakajima NK9 A Homare
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:manufacturer
|
gptkb:Nakajima_Aircraft_Company
|
|
gptkbp:max_speed
|
400 km/h
|
|
gptkbp:operational_history
|
gptkb:World_War_II
|
|
gptkbp:power_output
|
1,000 hp
|
|
gptkbp:production_years
|
1941-1945
|
|
gptkbp:propeller
|
variable-pitch propeller
|
|
gptkbp:replaced_by
|
gptkb:Mitsubishi_Kasei
|
|
gptkbp:successor
|
gptkb:Nakajima_NK9_H_Homare
|
|
gptkbp:torque
|
1,200 Nm
|
|
gptkbp:type
|
gptkb:radial_engine
|
|
gptkbp:used_in
|
gptkb:transport_aircraft
|
|
gptkbp:valve_configuration
|
overhead valves
|
|
gptkbp:variant
|
NK9 A, NK9 B
|
|
gptkbp:weight
|
400 kg
|
|
gptkbp:bfsParent
|
gptkb:Yokosuka_P1_Y
|
|
gptkbp:bfsLayer
|
4
|