Shvetsov ASh-82

GPTKB entity

Properties (63)
Predicate Object
gptkbp:instanceOf aircraft engine
gptkbp:application military aircraft
civil aircraft
gptkbp:bore 150 mm
gptkbp:compressionRatio 6.5:1
gptkbp:coolingSystem air-cooled
gptkbp:cylinderCount 14
gptkbp:displacement 41.5 L
gptkbp:drivetrain pushrod actuated
gptkbp:engine radial layout
Shvetsov_design
gptkbp:engineConfiguration horizontally opposed
over 10,000 units produced
gptkbp:engineType gptkb:ASh-82V
gptkb:ASh-82A
gptkb:ASh-82O
gptkb:ASh-82F
gptkb:ASh-82S
gptkb:ASh-82W
gptkb:ASh-82L
piston engine
ASh-82FN
ASh-82B
ASh-82C
ASh-82D
ASh-82E
ASh-82G
ASh-82H
ASh-82J
ASh-82K
ASh-82M
ASh-82T
ASh-82U
ASh-82N
ASh-82P
ASh-82Q
ASh-82R
ASh-82X
ASh-82Y
ASh-82Z
gptkbp:firstFlight 1940
gptkbp:fuelType spark ignition
aviation gasoline
carburetor
https://www.w3.org/2000/01/rdf-schema#label Shvetsov ASh-82
gptkbp:is_used_in gptkb:Ilyushin_Il-14
gptkb:Tupolev_Tu-2
Ilyushin Il-12
gptkbp:manufacturer gptkb:Shvetsov
gptkbp:notableUsers gptkb:Soviet_Air_Force
gptkb:Polish_Air_Force
gptkb:Czechoslovak_Air_Force
Aeroflot
gptkbp:performances high reliability
high power-to-weight ratio
moderate maintenance requirements
gptkbp:powerOutput 1,000 hp
gptkbp:productionYears 1940-1950
gptkbp:setting 14-cylinder
gptkbp:stroke 150 mm
gptkbp:successor gptkb:Shvetsov_ASh-73
gptkbp:type radial engine
gptkbp:weight 350 kg