|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Heinkel_He_70
gptkb:Ju_87_A
gptkb:Bf_108
|
|
gptkbp:aircraft_operated
|
gptkb:Junkers_Ju_88
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:bore
|
150 mm
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:cooling_system
|
liquid cooling
water-cooled
|
|
gptkbp:design
|
gptkb:Hugo_Junkers
|
|
gptkbp:displacement
|
20.7 L
|
|
gptkbp:engine
|
gptkb:Jumo_200_series
gptkb:engine
V-type
2,400 rpm
V12 layout
600 hp at 2,400 rpm
single-stage supercharger
|
|
gptkbp:engine_type
|
gptkb:Jumo_210_A
gptkb:Jumo_210_D
gptkb:Jumo_210_E
gptkb:Jumo_210_F
gptkb:Jumo_210_G
gptkb:Jumo_210_H
gptkb:Jumo_210_J
gptkb:Jumo_210_K
gptkb:Jumo_210_L
gptkb:Jumo_210_M
piston engine
reciprocating engine
|
|
gptkbp:first_flight
|
gptkb:1935
|
|
gptkbp:fuel_capacity
|
0.9 m
1.8 m
400 kg
|
|
gptkbp:fuel_type
|
gptkb:product
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Junkers Jumo 210
|
|
gptkbp:ignition_system
|
magneto ignition
|
|
gptkbp:is_designed_to
|
gptkb:aircraft
|
|
gptkbp:manufacturer
|
gptkb:Junkers
|
|
gptkbp:notable_users
|
gptkb:Luftwaffe
|
|
gptkbp:power_output
|
600 hp
|
|
gptkbp:production_years
|
1935-1945
|
|
gptkbp:propulsion
|
variable-pitch propeller
1.5 hp/kg
|
|
gptkbp:setting
|
gptkb:V12
|
|
gptkbp:stroke
|
150 mm
|
|
gptkbp:successor
|
gptkb:Jumo_211
|
|
gptkbp:torque
|
1,200 Nm
|
|
gptkbp:type
|
liquid-cooled V12 engine
|
|
gptkbp:used_in
|
gptkb:Junkers_Ju_87_Stuka
|
|
gptkbp:valve_configuration
|
overhead valves
|
|
gptkbp:weight
|
400 kg
|