|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
6
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|
gptkbp:bfsParent
|
gptkb:Junkers_Jumo_210
|
|
gptkbp:aircraft_operated
|
gptkb:Junkers_Ju_88
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:bore
|
130 mm
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:cooling_system
|
gptkb:fandom
water-cooled
water-cooled engine
|
|
gptkbp:design
|
gptkb:Hermann_Pohlmann
|
|
gptkbp:displacement
|
21.0 L
21,000 cm³
|
|
gptkbp:engine
|
gptkb:aircraft
gptkb:12
gptkb:Jumo_200_series
gptkb:Jumo_200_series_engines
gptkb:Junkers_Motorenbau_Gmb_H
high performance
V engine
high reliability
electric starter
inline engine
high reliability rating
produced in large numbers
2,400 rpm
V-12 configuration
600 hp at 2,400 rpm
important in WWII aviation history
|
|
gptkbp:engine_type
|
gptkb:Jumo_210_G
reciprocating engine
|
|
gptkbp:first_flight
|
1936
|
|
gptkbp:fuel_capacity
|
1,000 mm
400 kg
1,200 mm
1,800 mm
0.4 kg/hp/h
|
|
gptkbp:fuel_type
|
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Jumo 210 F
|
|
gptkbp:ignition_system
|
magneto ignition
|
|
gptkbp:is_designed_to
|
gptkb:aircraft
|
|
gptkbp:is_tested_for
|
extensively tested before production
|
|
gptkbp:maintenance
|
routine maintenance required
|
|
gptkbp:manufacturer
|
gptkb:Junkers
|
|
gptkbp:notable_users
|
gptkb:Luftwaffe
|
|
gptkbp:performance
|
high power-to-weight ratio
|
|
gptkbp:power_output
|
600 hp
|
|
gptkbp:production_years
|
1936-1945
|
|
gptkbp:setting
|
liquid-cooled
|
|
gptkbp:stroke
|
150 mm
|
|
gptkbp:successor
|
gptkb:Jumo_211
|
|
gptkbp:torque
|
1,200 Nm
pressure lubrication system
1,200 Nm at 2,400 rpm
|
|
gptkbp:type
|
V-12 engine
|
|
gptkbp:used_in
|
gptkb:Junkers_Ju_87_Stuka
|
|
gptkbp:weight
|
400 kg
|