Statements (31)
Predicate | Object |
---|---|
gptkbp:instanceOf |
piston engine
|
gptkbp:bore |
155.5 mm
|
gptkbp:compressionRatio |
6.3:1
|
gptkbp:configuration |
9-cylinder
|
gptkbp:coolingSystem |
air-cooled
|
gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
gptkbp:diameter |
1050 mm
|
gptkbp:displacement |
10.16 L
|
gptkbp:engineType |
piston engine
|
gptkbp:firstFlight |
1973
|
gptkbp:fuelType |
aviation gasoline
|
https://www.w3.org/2000/01/rdf-schema#label |
Vedeneyev M-14P
|
gptkbp:ignition |
dual magneto
|
gptkbp:length |
1000 mm
|
gptkbp:manufacturer |
gptkb:Vedeneyev
|
gptkbp:maximumSpeed |
2900 rpm
|
gptkbp:oilSystem |
dry sump
|
gptkbp:powerOutput |
360 hp
|
gptkbp:propulsion |
reduction gear
|
gptkbp:stroke |
155 mm
|
gptkbp:supercharger |
single-stage, single-speed
|
gptkbp:usedInAircraft |
gptkb:Yakovlev_Yak-52
gptkb:PZL-106_Kruk gptkb:Sukhoi_Su-26 gptkb:Sukhoi_Su-29 gptkb:Sukhoi_Su-31 |
gptkbp:valvetrain |
overhead valve
|
gptkbp:weight |
205 kg
|
gptkbp:bfsParent |
gptkb:Yakovlev_Yak-50
gptkb:Yakovlev_Yak-52 |
gptkbp:bfsLayer |
6
|