|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:Junkers_Jumo_213
|
|
gptkbp:aircraft_operated
|
gptkb:Junkers_Ju_88
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:cooling_system
|
liquid-cooled
water-cooled
|
|
gptkbp:design
|
gptkb:Junkers
|
|
gptkbp:displacement
|
22,500 cc
22.5 liters
|
|
gptkbp:engine
|
gptkb:Jumo_220_series
gptkb:12
gptkb:battle
various aircraft types
limited production
high reliability
high power-to-weight ratio
advanced for its time
V-12
1,000 horsepower
developed during WWII
dual ignition system
liquid-cooled V12
V-layout
influenced post-war engine designs
powerful and efficient
2,500 RPM
notable among WWII engines
part of German aviation advancements.
production difficulties during the war
specific to military use
|
|
gptkbp:engine_type
|
piston engine
Jumo 222 A, Jumo 222 B
|
|
gptkbp:first_flight
|
1939
|
|
gptkbp:fuel_capacity
|
800 mm
1,800 mm
|
|
gptkbp:fuel_type
|
gptkb:product
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Jumo 222
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:impact
|
significant in aviation history
|
|
gptkbp:is_designed_to
|
gptkb:aircraft
|
|
gptkbp:is_tested_for
|
extensively tested
|
|
gptkbp:maintenance
|
moderate maintenance required
|
|
gptkbp:manufacturer
|
gptkb:Junkers
|
|
gptkbp:notable_users
|
gptkb:Luftwaffe
|
|
gptkbp:origin
|
gptkb:government_agency
|
|
gptkbp:power_output
|
1,000 hp
|
|
gptkbp:production_years
|
1939-1945
|
|
gptkbp:setting
|
V engine
|
|
gptkbp:successor
|
Jumo 223
|
|
gptkbp:torque
|
1,200 Nm
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Junkers_Ju_87_Stuka
|
|
gptkbp:valve_configuration
|
overhead valves
|
|
gptkbp:weight
|
450 kg
|