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gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:bore
|
150 mm
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:configuration
|
14-cylinder
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gptkbp:cooling_system
|
air-cooled
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gptkbp:country_of_origin
|
gptkb:Soviet_Union
|
|
gptkbp:design_date
|
1939
|
|
gptkbp:engine
|
advanced for its time
multiple features for performance
used in several Soviet aircraft models
Shvetsov ASh-62
|
|
gptkbp:engine_configuration
|
radial
front-mounted
various modifications available
designed for durability
|
|
gptkbp:engine_displacement
|
30.5 L
|
|
gptkbp:engine_output
|
high output for its size
|
|
gptkbp:engine_power
|
high performance
high reliability
1,500 hours
good fuel efficiency
|
|
gptkbp:engine_specifications
|
detailed specifications available.
|
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gptkbp:engine_type
|
piston engine
compatible with multiple aircraft
|
|
gptkbp:first_flight
|
gptkb:1940
|
|
gptkbp:fuel_capacity
|
1,200 mm
|
|
gptkbp:fuel_type
|
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Shvetsov ASh-21
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:impact
|
significant impact on Soviet aviation
|
|
gptkbp:maintenance
|
periodic maintenance required
|
|
gptkbp:manufacturer
|
Shvetsov
|
|
gptkbp:noise_level
|
low vibration
moderate noise level
|
|
gptkbp:notable_users
|
gptkb:Soviet_Air_Force
|
|
gptkbp:power_output
|
1,000 hp
|
|
gptkbp:production_years
|
1940-1945
|
|
gptkbp:replaced_by
|
Shvetsov ASh-62
|
|
gptkbp:stroke
|
150 mm
|
|
gptkbp:successor
|
Shvetsov ASh-62
|
|
gptkbp:tuning
|
factory-tuned
|
|
gptkbp:type
|
gptkb:radial_engine
|
|
gptkbp:used_in
|
gptkb:Ilyushin_Il-4
|
|
gptkbp:valve_configuration
|
overhead valve
|
|
gptkbp:weight
|
400 kg
|
|
gptkbp:bfsParent
|
gptkb:La-9_fighter_aircraft
|
|
gptkbp:bfsLayer
|
6
|