Vedeneyev M14P radial engine
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:configuration |
9-cylinder
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:displacement |
10.16 liters
|
| gptkbp:engineType |
gptkb:piston_engine
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
avgas
|
| gptkbp:ignition |
dual magneto
|
| gptkbp:manufacturer |
gptkb:Vedeneyev
|
| gptkbp:maximumSpeed |
2900 rpm
|
| gptkbp:notableFor |
aerobatic aircraft use
|
| gptkbp:powerOutput |
360 hp
|
| gptkbp:supercharger |
yes
|
| gptkbp:usedInAircraft |
gptkb:Yakovlev_Yak-52
gptkb:Sukhoi_Su-26 gptkb:Sukhoi_Su-29 gptkb:Sukhoi_Su-31 |
| gptkbp:valveConfiguration |
overhead valve
|
| gptkbp:weight |
approximately 200 kg
|
| gptkbp:bfsParent |
gptkb:Yakovlev_Yak-55
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Vedeneyev M14P radial engine
|