Pratt & Whitney R-1340 radial engine
GPTKB entity
Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
5.75 in
|
| gptkbp:certification |
1925
|
| gptkbp:configuration |
single-row
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:displacement |
1,344 cubic inches
|
| gptkbp:engineType |
gptkb:piston_engine
|
| gptkbp:firstFlight |
1925
|
| gptkbp:fuelType |
aviation gasoline
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:nickname |
gptkb:Dragon
|
| gptkbp:notableFor |
first engine produced by Pratt & Whitney
first engine in the Wasp series |
| gptkbp:numberOfEngines |
9
|
| gptkbp:powerOutput |
up to 600 hp
|
| gptkbp:status |
historic
|
| gptkbp:stroke |
5.75 in
|
| gptkbp:usedBy |
gptkb:United_States_military
civil aviation |
| gptkbp:usedIn |
gptkb:North_American_T-6_Texan
gptkb:Douglas_DC-2 gptkb:Sikorsky_S-38 gptkb:Beechcraft_Model_18 gptkb:Grumman_Goose |
| gptkbp:weight |
650 lb (dry)
|
| gptkbp:bfsParent |
gptkb:de_Havilland_Canada_DHC-3_Otter
gptkb:North_American_R5T-1_Texan |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney R-1340 radial engine
|