Statements (32)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:basedOn |
gptkb:Wright_R-1820_Cyclone
|
| gptkbp:bore |
155 mm
|
| gptkbp:configuration |
piston engine
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
1,260 mm
|
| gptkbp:displacement |
29.87 L
|
| gptkbp:firstFlight |
1937
|
| gptkbp:fuelType |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Shvetsov ASh-62 engine
|
| gptkbp:length |
1,180 mm
|
| gptkbp:licenseProducedIn |
gptkb:China
gptkb:India gptkb:Poland |
| gptkbp:manufacturer |
gptkb:Shvetsov
|
| gptkbp:numberOfEngines |
9
|
| gptkbp:otherName |
gptkb:M-62
HS-62 Zhuzhou HS-5 |
| gptkbp:powerOutput |
1000 hp
|
| gptkbp:stroke |
174 mm
|
| gptkbp:successor |
gptkb:Shvetsov_ASh-82
|
| gptkbp:supercharger |
single-stage
|
| gptkbp:usedInAircraft |
gptkb:Antonov_An-2
gptkb:Lisunov_Li-2 gptkb:Yakovlev_Yak-12 gptkb:Polikarpov_Po-2 gptkb:PZL-104_Wilga |
| gptkbp:weight |
510 kg
|
| gptkbp:bfsParent |
gptkb:Vladimir_N._Shvetsov
|
| gptkbp:bfsLayer |
7
|