Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
155.5 mm
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:developedBy |
gptkb:Shvetsov_ASh-82
|
| gptkbp:displacement |
41.2 L
|
| gptkbp:engineType |
14-cylinder, two-row, air-cooled radial engine
|
| gptkbp:firstFlight |
1942
|
| gptkbp:fuelType |
aviation gasoline
|
| gptkbp:manufacturer |
gptkb:Shvetsov_Design_Bureau
|
| gptkbp:notableFeature |
direct fuel injection
improved high-altitude performance |
| gptkbp:powerOutput |
1850 hp
|
| gptkbp:stroke |
155 mm
|
| gptkbp:supercharger |
single-stage, two-speed
|
| gptkbp:usedDuring |
gptkb:World_War_II
|
| gptkbp:usedInAircraft |
gptkb:Lavochkin_La-5FN
gptkb:Tupolev_Tu-2 gptkb:Sukhoi_Su-2 gptkb:Lavochkin_La-7 |
| gptkbp:weight |
970 kg
|
| gptkbp:bfsParent |
gptkb:Ла-7
|
| gptkbp:bfsLayer |
8
|
| http://www.w3.org/2000/01/rdf-schema#label |
Швецов АШ-82ФН
|