Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
light helicopters
light fixed-wing aircraft |
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:diameter |
13.8 in
|
| gptkbp:family |
gptkb:Allison_Model_250
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
gptkb:gasoline
|
| gptkbp:length |
40.5 in
|
| gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
| gptkbp:marketedAs |
gptkb:Rolls-Royce_250-C20
|
| gptkbp:numberOfStages |
2
7 axial, 1 centrifugal |
| gptkbp:powerOutput |
420 shp
|
| gptkbp:successor |
gptkb:Rolls-Royce_250-C30
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedIn |
gptkb:Agusta_A109
gptkb:Hughes_500 gptkb:Bell_206_JetRanger gptkb:Schweizer_330 |
| gptkbp:weight |
170 lb
|
| gptkbp:bfsParent |
gptkb:Bell_206
gptkb:Bo_105 gptkb:Bell_206_JetRanger gptkb:Bell_206B_JetRanger |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Allison 250-C20
|