Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Robinson_R66
|
| gptkbp:basedOn |
gptkb:Rolls-Royce_Model_250
|
| gptkbp:certification |
gptkb:FAA
|
| gptkbp:compressionRatio |
centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
19.0 in
|
| gptkbp:firstRun |
2001
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce RR300
|
| gptkbp:introduced |
2007
|
| gptkbp:length |
39.0 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:marketedAs |
light helicopters
|
| gptkbp:powerOutput |
300 shp
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedIn |
helicopters
|
| gptkbp:weight |
204 lb
|
| gptkbp:bfsParent |
gptkb:Robinson_R66
|
| gptkbp:bfsLayer |
7
|