Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:Agusta_A109
gptkb:Hughes_500 gptkb:Bell_206_JetRanger |
| gptkbp:compressionRatio |
centrifugal
|
| gptkbp:configuration |
single-shaft
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
13.8 in
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:length |
39.0 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
gptkb:Allison_Engine_Company |
| gptkbp:partOfSeries |
gptkb:Rolls-Royce_Model_250
|
| gptkbp:powerOutput |
420 shp
|
| gptkbp:successor |
gptkb:Rolls-Royce_250-C30
|
| gptkbp:usedIn |
fixed-wing aircraft
light helicopters |
| gptkbp:weight |
141 lb
|
| gptkbp:bfsParent |
gptkb:Allison_250-C20
gptkb:Allison_250-B17C |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce 250-C20
|