Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bore |
155.5 mm
|
| gptkbp:compressionRatio |
6.4:1
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:Poland
|
| gptkbp:derivedFrom |
gptkb:Shvetsov_ASh-62
|
| gptkbp:diameter |
1,260 mm
|
| gptkbp:displacement |
29.87 L
|
| gptkbp:firstFlight |
1940s
|
| gptkbp:fuelType |
aviation gasoline
270 g/hp·h |
| https://www.w3.org/2000/01/rdf-schema#label |
ASz-62IR
|
| gptkbp:length |
1,180 mm
|
| gptkbp:manufacturer |
Wytwórnia Sprzętu Komunikacyjnego (WSK) Kalisz
|
| gptkbp:numberOfEngines |
9
|
| gptkbp:powerOutput |
1000 hp
|
| gptkbp:stroke |
174.5 mm
|
| gptkbp:supercharger |
single-stage, single-speed
|
| gptkbp:type |
piston engine
|
| gptkbp:usedInAircraft |
gptkb:Antonov_An-2
gptkb:PZL_M-18_Dromader |
| gptkbp:weight |
510 kg
|
| gptkbp:bfsParent |
gptkb:Shvetsov_ASh-62_radial_engine
|
| gptkbp:bfsLayer |
7
|