Junkers Jumo 210

GPTKB entity

Statements (55)
Predicate Object
gptkbp:instance_of gptkb:jet_engine
gptkbp:application gptkb:military_aircraft
gptkbp:bore 150 mm
gptkbp:compression_ratio 6.5:1
gptkbp:configuration gptkb:V12
gptkbp:cooling_system liquid cooling
water-cooled
gptkbp:design gptkb:Hugo_Junkers
gptkbp:displacement 20.7 L
gptkbp:engine gptkb:Jumo_200_series
single-stage supercharger
gptkbp:engine_configuration gptkb:V8_engine
V-type
V12 layout
gptkbp:engine_displacement 20.7 L
gptkbp:engine_power 2,400 rpm
600 hp at 2,400 rpm
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:carburetor
aviation gasoline
https://www.w3.org/2000/01/rdf-schema#label Junkers Jumo 210
gptkbp:ignition_system magneto ignition
gptkbp:intended_use gptkb:fighter_aircraft
gptkbp:manufacturer gptkb:Junkers
gptkbp:notable_users gptkb:Luftwaffe
gptkbp:power_output 600 hp
gptkbp:production_years 1935-1945
gptkbp:propeller variable-pitch propeller
gptkbp:propulsion 1.5 hp/kg
gptkbp:related_aircraft gptkb:Junkers_Ju_88
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
gptkbp:bfsParent gptkb:Heinkel_He_70
gptkb:Ju_87_A
gptkbp:bfsLayer 5