Statements (16)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:configuration |
axial-centrifugal flow
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:firstFlight |
1955
|
| gptkbp:fuelType |
gptkb:gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming T53-L-1 turboshaft
|
| gptkbp:intendedUse |
gptkb:helicopter
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:numberOfStages |
2
5 |
| gptkbp:powerOutput |
860 shp
|
| gptkbp:usedIn |
gptkb:Bell_205
gptkb:Bell_204 gptkb:Bell_UH-1_Iroquois |
| gptkbp:bfsParent |
gptkb:UH-1A
|
| gptkbp:bfsLayer |
7
|