Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:certification |
1997
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
13.8 in
|
| gptkbp:family |
gptkb:Rolls-Royce_Model_250
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:length |
39.0 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:powerOutput |
650 shp
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedIn |
gptkb:Bell_407
gptkb:MD_Helicopters_MD_600N gptkb:Schweizer_S-333 |
| gptkbp:weight |
152 lb
|
| gptkbp:bfsParent |
gptkb:Bell_407
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce 250-C47B
|