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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:application
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gptkb:military_aircraft
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gptkbp:bore
|
150 mm
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|
gptkbp:compression_ratio
|
6.5:1
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gptkbp:configuration
|
liquid-cooled
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|
gptkbp:control_system
|
mechanical throttle
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gptkbp:cooling_system
|
liquid cooling
water-cooled
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|
gptkbp:displacement
|
21.0 L
|
|
gptkbp:engine
|
performance upgrades
various aircraft types
mass production
four-stroke
influenced future designs
historically significant engine
context in aviation history
contributed to advancements in technology
operational use in WWII
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|
gptkbp:engine_configuration
|
V-type
aerodynamic efficiency
V engine
detailed specifications available
reflects design philosophy of the era
cradle mount
notable characteristics documented
|
|
gptkbp:engine_performance_evaluation
|
evaluated for performance
|
|
gptkbp:engine_power
|
high reliability
high power-to-weight ratio
limited lifespan
performance metrics recorded
|
|
gptkbp:engine_production_facilities
|
produced in multiple facilities
|
|
gptkbp:engine_specifications_documentation
|
documented specifications available
|
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gptkbp:engine_type
|
gptkb:Jumo_210_Da
|
|
gptkbp:first_flight
|
1936
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|
gptkbp:fuel_type
|
aviation gasoline
carbureted
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Jumo 210 H
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:intended_use
|
gptkb:fighter_aircraft
|
|
gptkbp:is_tested_for
|
ground testing
used in various testing facilities
|
|
gptkbp:maintenance
|
moderate maintenance
|
|
gptkbp:manufacturer
|
gptkb:Junkers
|
|
gptkbp:notable_feature
|
gptkb:Racing
|
|
gptkbp:number_of_engines
|
gptkb:12
|
|
gptkbp:power_output
|
600 hp
|
|
gptkbp:production_years
|
1936-1945
|
|
gptkbp:propeller
|
variable-pitch propeller
|
|
gptkbp:related_aircraft
|
gptkb:Junkers_Ju_88
|
|
gptkbp:replaced_by
|
gptkb:Jumo_213
|
|
gptkbp:stroke
|
150 mm
|
|
gptkbp:successor
|
gptkb:Jumo_211
|
|
gptkbp:type
|
V-12 engine
|
|
gptkbp:used_in
|
gptkb:Junkers_Ju_87
|
|
gptkbp:weight
|
400 kg
|
|
gptkbp:bfsParent
|
gptkb:Junkers_Jumo_210
|
|
gptkbp:bfsLayer
|
6
|