Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:alsoKnownAs |
gptkb:Rolls-Royce_M250
|
| gptkbp:application |
helicopters
fixed-wing aircraft |
| gptkbp:certification |
1965
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
19.0 in
|
| gptkbp:firstFlight |
1961
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Allison 250
|
| gptkbp:length |
39.0 in
|
| gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
| gptkbp:marketedAs |
gptkb:Rolls-Royce
|
| gptkbp:numberBuilt |
over 30,000
|
| gptkbp:powerOutput |
420 shp
|
| gptkbp:successor |
gptkb:Rolls-Royce_M250
|
| gptkbp:type |
turboprop
turboshaft |
| gptkbp:usedIn |
gptkb:Agusta_A109
gptkb:Bell_206_JetRanger gptkb:Eurocopter_AS355 gptkb:MD_Helicopters_MD_500 gptkb:Schweizer_330 |
| gptkbp:weight |
170 lb
|
| gptkbp:bfsParent |
gptkb:Allison_Engine_Company
|
| gptkbp:bfsLayer |
6
|