BMW 802

GPTKB entity

Statements (53)
Predicate Object
gptkbp:instance_of gptkb:jet_engine
gptkbp:application gptkb:military_aircraft
gptkbp:bore 150 mm
gptkbp:compression_ratio 6.5:1
gptkbp:configuration 9-cylinder
gptkbp:cooling_system air-cooled
gptkbp:country_of_origin gptkb:Germany
gptkbp:design Hermann W. H. von Schenk
gptkbp:displacement 41.5 liters
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
gptkbp:engine_configuration 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
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
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