Jumo 210 M

URI: https://gptkb.org/entity/Jumo_210_M
GPTKB entity
Statements (52)
Predicate Object
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 gptkb:fandom
liquid-cooled
water-cooled
gptkbp:displacement 21.0 L
gptkbp:engine gptkb:Junkers_Ju_88
gptkb:Jumo_211
high reliability
advanced for its time
good fuel efficiency
influenced later designs
developed in the 1930s
2,400 rpm
V-12 configuration
V-12 layout
two-stage supercharger
powerful and compact
600 hp at 2,400 rpm
single-stage supercharger
liquid-cooled V engine
V-12, liquid-cooled
produced until 1940
used in various aircraft.
gptkbp:engine_type gptkb:Jumo_210_G
piston engine
gptkbp:first_flight 1936
gptkbp:fuel_capacity 1,000 mm
400 kg
1,200 mm
1,800 mm
gptkbp:fuel_type gptkb:product
aviation gasoline
https://www.w3.org/2000/01/rdf-schema#label Jumo 210 M
gptkbp:ignition_system magneto ignition
gptkbp:manufacturer gptkb:Junkers
gptkbp:notable_users gptkb:Luftwaffe
gptkbp:power_output 600 hp
gptkbp:produced_by approximately 10,000
gptkbp:production_years 1936-1940
gptkbp:setting V engine
gptkbp:stroke 150 mm
gptkbp:successor gptkb:Jumo_211
gptkbp:torque 1,200 Nm
gptkbp:type V-12 engine
gptkbp:used_in gptkb:Junkers_Ju_87_Stuka
gptkbp:valve_configuration overhead valves
gptkbp:weight 400 kg