Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
5.75 in
|
| gptkbp:category |
aircraft piston engines
|
| gptkbp:compressionRatio |
5.25:1
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
51.5 in
|
| gptkbp:displacement |
1,344 cu in
|
| gptkbp:engineType |
gptkb:piston_engine
|
| gptkbp:firstFlight |
1925
|
| gptkbp:fuelType |
aviation gasoline
|
| gptkbp:introduced |
1926
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:notableFor |
first engine produced by Pratt & Whitney
|
| gptkbp:numberOfEngines |
9
|
| gptkbp:powerOutput |
up to 600 hp
|
| gptkbp:status |
retired
|
| gptkbp:stroke |
5.75 in
|
| gptkbp:successor |
gptkb:Pratt_&_Whitney_R-1340_Wasp
|
| gptkbp:usedIn |
gptkb:Boeing_Stearman
gptkb:Douglas_DC-2 gptkb:Lockheed_Vega gptkb:Grumman_Goose gptkb:Curtiss_P-36_Hawk |
| gptkbp:weight |
650 lb (dry)
|
| gptkbp:bfsParent |
gptkb:Boeing_247
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Wasp
|