Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Gulfstream_GIV
|
| gptkbp:bypassRatio |
3.1:1
|
| gptkbp:compressionRatio |
2-stage fan, 12-stage HP compressor
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
1.04 m
|
| gptkbp:family |
gptkb:Rolls-Royce_Tay
|
| gptkbp:firstFlight |
1985
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:hasTower |
2-stage HP, 3-stage LP
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Tay 611-8C
|
| gptkbp:length |
2.6 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_plc
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
13,850 lbf
|
| gptkbp:weight |
1,350 kg
|
| gptkbp:bfsParent |
gptkb:Gulfstream_G350
gptkb:Gulfstream_G450 |
| gptkbp:bfsLayer |
7
|