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gptkbp:instance_of
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gptkb:engine
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gptkbp:bfsLayer
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6
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gptkbp:bfsParent
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gptkb:Junkers_Jumo_210
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gptkbp:application
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gptkb:aircraft
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gptkbp:bore
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150 mm
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gptkbp:compression_ratio
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6.5:1
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gptkbp:cooling_system
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Liquid-cooled
Water-cooled
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gptkbp:displacement
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21.0 L
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gptkbp:drivetrain
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Reduction gearbox
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gptkbp:engine
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gptkb:12
High reliability
Electric starter
Supercharged
1,000 hours
Good performance at altitude
Nose-mounted
Influenced later German aircraft engines.
Various modifications during production
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gptkbp:engine_type
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Compatible with various aircraft designs
Jumo 210 D, Jumo 210 E
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gptkbp:fuel_capacity
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1,000 mm
1,200 mm
1,800 mm
Moderate fuel efficiency
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gptkbp:fuel_type
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gptkb:product
Benzin
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|
https://www.w3.org/2000/01/rdf-schema#label
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Jumo 210 L
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gptkbp:ignition_system
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Magneto ignition
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gptkbp:maintenance
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Moderate maintenance required
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gptkbp:manufacturer
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gptkb:Junkers
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gptkbp:noise_level
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Low vibration
Moderate noise level
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gptkbp:original_run
|
1938
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gptkbp:power_output
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600 hp
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gptkbp:production_years
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1938-1945
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gptkbp:propulsion
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Variable-pitch propeller
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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:tuning
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Tuned for high altitude
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gptkbp:type
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V-12 engine
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gptkbp:used_in
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gptkb:Junkers_Ju_87_Stuka
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gptkbp:valve_configuration
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Overhead valve
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gptkbp:weight
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400 kg
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