Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:alsoKnownAs |
gptkb:Allison_Model_250
|
| gptkbp:application |
gptkb:helicopter
fixed-wing aircraft |
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:firstFlight |
1961
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Model 250
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
gptkb:Allison_Engine_Company |
| gptkbp:notableVariant |
Model 250-B17
Model 250-C20 Model 250-C30 Model 250-C47 |
| gptkbp:numberBuilt |
over 30,000
|
| gptkbp:powerOutput |
317 to 715 shaft horsepower
|
| gptkbp:type |
turboprop
turboshaft |
| gptkbp:usedIn |
gptkb:Bell_206
gptkb:Eurocopter_AS355 gptkb:MD_Helicopters_MD_500 gptkb:Schweizer_333 AgustaWestland AW119 |
| gptkbp:bfsParent |
gptkb:Rolls-Royce_250-C30P
gptkb:Rolls-Royce_250-C47B gptkb:Rolls-Royce_Defence gptkb:Rolls-Royce_250-C20W gptkb:Rolls-Royce_250-C20W_turboshaft |
| gptkbp:bfsLayer |
7
|