Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
gptkb:gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce 250-C30
|
| gptkbp:introducedIn |
1976
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
gptkb:Allison_Engine_Company |
| gptkbp:numberOfStages |
2
7 axial, 1 centrifugal |
| gptkbp:partOfSeries |
gptkb:Rolls-Royce_Model_250
|
| gptkbp:powerOutput |
650 shp
|
| gptkbp:successor |
Rolls-Royce 250-C40
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedInAircraft |
gptkb:Bell_206L_LongRanger
gptkb:MBB_Bo_105 gptkb:Hughes_500D |
| gptkbp:bfsParent |
gptkb:Allison_250-C20
gptkb:Allison_250-C20_turboshaft |
| gptkbp:bfsLayer |
7
|