Pratt & Whitney Wasp radial engine
GPTKB entity
Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
5.75 inches
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:displacement |
1,344 cubic inches
|
| gptkbp:engineType |
gptkb:piston_engine
|
| gptkbp:firstFlight |
1925
|
| gptkbp:fuelType |
aviation gasoline
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:notableFor |
first engine produced by Pratt & Whitney
widely used in 1920s and 1930s aircraft |
| gptkbp:numberOfEngines |
9
|
| gptkbp:powerOutput |
up to 600 hp
|
| gptkbp:stroke |
5.75 inches
|
| gptkbp:successor |
gptkb:Pratt_&_Whitney_R-1340_Wasp
|
| gptkbp:usedInAircraft |
gptkb:Boeing_Stearman
gptkb:Douglas_DC-2 gptkb:Lockheed_Vega gptkb:Grumman_Goose |
| gptkbp:weight |
approximately 650 lbs
|
| gptkbp:bfsParent |
gptkb:Fairchild_71B
gptkb:Fairchild_71C |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Wasp radial engine
|