Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Bombardier_Global_5000
gptkb:Gulfstream_G500 gptkb:Bombardier_Global_Express gptkb:Gulfstream_G550 |
| gptkbp:bypassRatio |
4.2:1
|
| gptkbp:compressor_type |
2-stage fan, 10-stage HP compressor
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
0.97 m
|
| 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 BR710A2-20
|
| gptkbp:length |
2.59 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_plc
|
| gptkbp:number_of_shafts |
2
|
| gptkbp:thrust |
15,500 lbf
|
| gptkbp:turbineType |
2-stage HP, 2-stage LP
|
| gptkbp:weight |
1,580 kg
|
| gptkbp:bfsParent |
gptkb:Bombardier_Global_5000
gptkb:Bombardier_Global_6000 |
| gptkbp:bfsLayer |
6
|