|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:Jumo_200_series
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:bore
|
150 mm
150 millimeters
|
|
gptkbp:compression_ratio
|
16:1
|
|
gptkbp:cooling_system
|
gptkb:item
liquid-cooled
liquid-cooled system
|
|
gptkbp:displacement
|
30.5 L
30.5 liters
|
|
gptkbp:engine
|
gptkb:Jumo_200_A-1
gptkb:12
gptkb:Junkers_Gmb_H
V engine
four-stroke
600 horsepower
V-type engine
V12 configuration
2200 rpm
used in various aircraft.
military aircraft application
|
|
gptkbp:engine_type
|
reciprocating engine
diesel engine type
|
|
gptkbp:first_flight
|
1934
|
|
gptkbp:fuel_capacity
|
0.9 m
1.8 m
400 kilograms
200 g/k Wh
|
|
gptkbp:fuel_type
|
diesel
direct injection
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Jumo 200 A
|
|
gptkbp:ignition_system
|
compression ignition
|
|
gptkbp:manufacturer
|
gptkb:Junkers
|
|
gptkbp:operational_area
|
gptkb:World_War_II
|
|
gptkbp:power_output
|
600 hp
|
|
gptkbp:production_years
|
1934-1940
|
|
gptkbp:setting
|
gptkb:V12
|
|
gptkbp:stroke
|
180 mm
180 millimeters
|
|
gptkbp:successor
|
gptkb:Jumo_205
|
|
gptkbp:torque
|
1500 Nm
1500 Newton-meters
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Junkers_Ju_86
|
|
gptkbp:valve_configuration
|
overhead valves
|
|
gptkbp:weight
|
400 kg
|