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
|
9-cylinder
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gptkbp:cooling_system
|
air-cooled
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gptkbp:country_of_origin
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gptkb:Germany
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gptkbp:design
|
Hermann W. H. von Schenk
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gptkbp:displacement
|
41.5 liters
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gptkbp:engine
|
used in various aircraft models
influenced future aircraft engine designs
BMW 800 series
faced challenges during production due to war conditions
incorporated innovative technologies for its time
part of BMW's aviation history
produced in large numbers during WWII
notable features include high power-to-weight ratio
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gptkbp:engine_configuration
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radial
horizontally opposed
detailed specifications available
aircraft engine design
|
gptkbp:engine_contributions
|
contributed to the advancement of aviation technology.
|
gptkbp:engine_displacement
|
41,500 cc
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gptkbp:engine_power
|
high performance
high reliability
good fuel efficiency
1,000 hp at 2,000 RPM
|
gptkbp:engine_type
|
piston engine
several variants developed
|
gptkbp:first_introduced
|
1930s
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gptkbp:fuel_capacity
|
300 kg
|
gptkbp:fuel_type
|
gptkb:carburetor
aviation gasoline
|
https://www.w3.org/2000/01/rdf-schema#label
|
BMW 802
|
gptkbp:ignition_system
|
magneto
|
gptkbp:is_tested_for
|
extensively tested during development
|
gptkbp:manufacturer
|
gptkb:BMW
|
gptkbp:max_speed
|
2,000
|
gptkbp:notable_users
|
gptkb:Junkers_Ju_90
|
gptkbp:number_of_engines
|
gptkb:9
|
gptkbp:power_output
|
1,000 hp
|
gptkbp:production_years
|
1935-1945
|
gptkbp:propeller
|
variable pitch
|
gptkbp:replaced_by
|
gptkb:BMW_801
|
gptkbp:stroke
|
160 mm
|
gptkbp:successor
|
gptkb:BMW_801
|
gptkbp:torque
|
1,500 Nm
|
gptkbp:type
|
gptkb:radial_engine
|
gptkbp:used_in
|
gptkb:aircraft
|
gptkbp:valve_configuration
|
pushrod
|
gptkbp:weight
|
300 kg
|
gptkbp:bfsParent
|
gptkb:BMW_801
|
gptkbp:bfsLayer
|
5
|