Statements (16)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:displacement |
1,344 in³
|
| gptkbp:engineType |
gptkb:piston_engine
|
| gptkbp:firstFlight |
1925
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:numberOfEngines |
9
|
| gptkbp:powerOutput |
425 hp
|
| gptkbp:successor |
gptkb:Pratt_&_Whitney_R-1340_Wasp
|
| gptkbp:usedIn |
gptkb:Douglas_O-2
Boeing F2B Curtiss Falcon |
| gptkbp:bfsParent |
gptkb:Wasp_flamethrower_carrier
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Wasp Mk I
|