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gptkbp:instance_of
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gptkb:engine
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gptkbp:bfsLayer
|
6
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gptkbp:bfsParent
|
gptkb:Junkers_Jumo_210
gptkb:Jumo_205
gptkb:Jumo_210
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|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:certification
|
certified for use
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|
gptkbp:compression_ratio
|
16:1
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gptkbp:cooling_system
|
liquid-cooled
water-cooled
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|
gptkbp:displacement
|
30 L
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gptkbp:engine
|
gptkb:aircraft
gptkb:advanced_technology
gptkb:12
gptkb:Jumo_200
gptkb:Jumo_205
mass production
V engine
high reliability
four-stroke
high efficiency
innovative design
influential in aviation history
inline engine
V-type engine
part of aviation history
detailed specifications available
continuous development
2300 rpm
600 hp at 2300 rpm
characteristics include power and efficiency
notable features include durability
widely used in WWII aircraft
|
|
gptkbp:engine_type
|
gptkb:Jumo_200_A
gptkb:Jumo_200_D
reciprocating engine
multiple variants produced
|
|
gptkbp:first_flight
|
1934
|
|
gptkbp:fuel_capacity
|
0.9 m
2.5 m
1.2 m
200 g/k Wh
|
|
gptkbp:fuel_type
|
diesel
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Jumo 200 series
|
|
gptkbp:impact
|
significant impact on aircraft design.
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:maintenance
|
low maintenance
|
|
gptkbp:manufacturer
|
gptkb:Junkers
|
|
gptkbp:notable_users
|
gptkb:Luftwaffe
|
|
gptkbp:power_output
|
600 hp
|
|
gptkbp:production_years
|
1934-1940
|
|
gptkbp:setting
|
V-12
|
|
gptkbp:successor
|
gptkb:Jumo_204
|
|
gptkbp:torque
|
2000 Nm
2000 Nm at 1500 rpm
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Junkers_Ju_86
|
|
gptkbp:weight
|
400 kg
|