Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:bypassRatio |
4.4:1
|
| gptkbp:certification |
1998
|
| gptkbp:configuration |
two-shaft
|
| gptkbp:countryOfOrigin |
gptkb:Germany
|
| gptkbp:family |
gptkb:Rolls-Royce_BR700
|
| gptkbp:firstRun |
1995
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce BR715
|
| gptkbp:length |
2.6 m
|
| gptkbp:mainRotorDiameter |
137 cm
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Deutschland
|
| gptkbp:numberOfStages |
2
8 |
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:Rolls-Royce_Tay
|
| gptkbp:thrust |
14,000–21,000 lbf
|
| gptkbp:usedInAircraft |
gptkb:Boeing_717
|
| gptkbp:weight |
1,800 kg
|
| gptkbp:bfsParent |
gptkb:Boeing_717
gptkb:Boeing_717-200 |
| gptkbp:bfsLayer |
6
|