|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:certification
|
military certification
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:configuration
|
9-cylinder
|
|
gptkbp:control_system
|
mechanical
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:country_of_origin
|
gptkb:Japan
|
|
gptkbp:design_date
|
1939
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:displacement
|
1,000 cubic inches
|
|
gptkbp:engine
|
gptkb:fighter_aircraft
gptkb:historical_significance
electric starter
|
|
gptkbp:engine_configuration
|
Japanese design
radial
horizontally opposed
|
|
gptkbp:engine_finish
|
aluminum alloy
|
|
gptkbp:engine_power
|
high performance
high reliability
good efficiency
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1940
|
|
gptkbp:fuel_capacity
|
150 kg
|
|
gptkbp:fuel_economy
|
200 L/h
|
|
gptkbp:fuel_type
|
aviation gasoline
carbureted
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Nakajima NK9 A
|
|
gptkbp:ignition_system
|
magneto
|
|
gptkbp:is_tested_for
|
ground testing
|
|
gptkbp:length
|
1,200 mm
|
|
gptkbp:maintenance
|
100 hours
|
|
gptkbp:manufacturer
|
gptkb:Nakajima_Aircraft_Company
|
|
gptkbp:number_of_engines
|
gptkb:9
|
|
gptkbp:operational_history
|
gptkb:World_War_II
|
|
gptkbp:power_output
|
1,000 hp
|
|
gptkbp:produces
|
1,500 units
|
|
gptkbp:production_years
|
1940-1945
|
|
gptkbp:propeller
|
variable-pitch
|
|
gptkbp:related_aircraft
|
gptkb:Nakajima_Ki-84
|
|
gptkbp:successor
|
gptkb:Nakajima_NK9_H
|
|
gptkbp:torque
|
1,200 Nm
|
|
gptkbp:type
|
gptkb:radial_engine
|
|
gptkbp:used_in
|
gptkb:Nakajima_Ki-43
|
|
gptkbp:weight
|
300 kg
|
|
gptkbp:bfsParent
|
gptkb:Nakajima_B5_N
|
|
gptkbp:bfsLayer
|
5
|