Pratt & Whitney R-1340-18 Wasp radial engine
GPTKB entity
Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| 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
used in both military and civilian aircraft |
| gptkbp:numberOfEngines |
9
|
| gptkbp:powerOutput |
up to 600 hp
|
| gptkbp:usedIn |
gptkb:North_American_T-6_Texan
gptkb:Grumman_G-21_Goose gptkb:Beechcraft_Model_18 |
| gptkbp:bfsParent |
gptkb:Curtiss_SOC_Seagull
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney R-1340-18 Wasp radial engine
|