Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Let_L-410
Thrush 510G Technoavia Rysachok |
| gptkbp:certification |
gptkb:EASA
gptkb:FAA |
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
single-shaft
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:derivedFrom |
gptkb:Walter_M601
|
| gptkbp:firstFlight |
2010
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
GE H80 turboprop
|
| gptkbp:introducedIn |
2012
|
| gptkbp:manufacturer |
gptkb:GE_Aviation
|
| gptkbp:marketedAs |
GE H Series
|
| gptkbp:numberOfStages |
1
2 axial, 1 centrifugal |
| gptkbp:powerOutput |
800 shp
|
| gptkbp:type |
piston engine
|
| gptkbp:bfsParent |
gptkb:Aero_L-410_Turbolet
|
| gptkbp:bfsLayer |
7
|