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gptkbp:instance_of
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gptkb:engine
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gptkbp:application
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gptkb:aircraft
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gptkbp:bore
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130 mm
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gptkbp:certification
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military certification required
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gptkbp:compression_ratio
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6.5:1
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gptkbp:cooling_system
|
liquid cooling
liquid-cooled
water-cooled
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gptkbp:displacement
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21.0 L
21,000 cc
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gptkbp:emissions_standard
|
standard emissions for the time
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|
gptkbp:engine
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gptkb:Jumo_200_series
gptkb:battle
high reliability
four-stroke
naturally aspirated
various aircraft models
1936-1945
V-12
moderate efficiency
V layout
liquid-cooled V-12
600 hp at 2,400 rpm
various upgrades during production
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gptkbp:engine_type
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multiple variants developed.
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gptkbp:first_flight
|
1936
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gptkbp:fuel_capacity
|
800 mm
1,800 mm
0.4 kg/hp/hr
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gptkbp:fuel_type
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gptkb:product
aviation gasoline
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|
https://www.w3.org/2000/01/rdf-schema#label
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Jumo 210 E
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gptkbp:ignition_system
|
magneto
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gptkbp:is_tested_for
|
extensively tested before production
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gptkbp:maintenance
|
moderate maintenance required
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gptkbp:manufacturer
|
gptkb:Junkers
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gptkbp:noise_level
|
low vibration
moderate noise
|
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gptkbp:notable_users
|
gptkb:Luftwaffe
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gptkbp:number_built
|
approximately 10,000
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gptkbp:power_output
|
600 hp
|
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gptkbp:propulsion
|
variable-pitch
1.5 hp/kg
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gptkbp:retirement_year
|
1945
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gptkbp:setting
|
V engine
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gptkbp:stroke
|
150 mm
|
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gptkbp:successor
|
gptkb:Jumo_211
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|
gptkbp:torque
|
1,200 Nm
wet sump
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gptkbp:type
|
V-12 engine
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|
gptkbp:used_in
|
gptkb:Junkers_Ju_87_Stuka
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gptkbp:valve_configuration
|
overhead valves
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gptkbp:weight
|
400 kg
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gptkbp:year_created
|
1936
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gptkbp:bfsParent
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gptkb:Junkers_Jumo_210
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gptkbp:bfsLayer
|
6
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