Statements (31)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb: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 |
gptkb:piston_engine
|
| gptkbp:firstFlight |
1973
|
| gptkbp:fuelType |
aviation gasoline
|
| 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 |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
Vedeneyev M-14P
|