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gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Junkers_Jumo_210
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:bore
|
130 mm
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:cooling_system
|
Water-cooled
Liquid-cooled engine
Liquid cooling system
|
|
gptkbp:displacement
|
21.0 L
|
|
gptkbp:engine
|
gptkb:aircraft
gptkb:12
V engine
600 horsepower
V-12 configuration
Fuselage-mounted
|
|
gptkbp:engine_type
|
Piston engine
|
|
gptkbp:first_flight
|
1936
|
|
gptkbp:fuel_capacity
|
0.9 m
1.8 m
0.5 m
400 kg
0.8 m
|
|
gptkbp:fuel_type
|
gptkb:product
Benzin
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Jumo 210 D
|
|
gptkbp:ignition_system
|
Magneto ignition
|
|
gptkbp:manufacturer
|
gptkb:Junkers
|
|
gptkbp:max_speed
|
2800
|
|
gptkbp:operational_history
|
gptkb:World_War_II
|
|
gptkbp:power_output
|
600 hp
|
|
gptkbp:production_years
|
1936-1940
|
|
gptkbp:propulsion
|
Variable-pitch propeller
|
|
gptkbp:setting
|
Liquid-cooled
|
|
gptkbp:stroke
|
150 mm
|
|
gptkbp:successor
|
gptkb:Jumo_211
|
|
gptkbp:torque
|
1200 Nm
|
|
gptkbp:type
|
V-12 engine
|
|
gptkbp:used_in
|
gptkb:Junkers_Ju_87_Stuka
|
|
gptkbp:valve_configuration
|
Overhead valves
|
|
gptkbp:variant
|
gptkb:Jumo_210_G
|
|
gptkbp:weight
|
400 kg
|