Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:bypassRatio |
8.7:1
|
| gptkbp:certification |
gptkb:FAA
|
| gptkbp:competition |
gptkb:Rolls-Royce_Trent_900
|
| gptkbp:compressionRatio |
23:1
|
| gptkbp:configuration |
dual-spool
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:General_Electric
gptkb:Pratt_&_Whitney |
| gptkbp:firstRun |
2004
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Engine Alliance GP7200
|
| gptkbp:length |
184 in
|
| gptkbp:mainRotorDiameter |
112 in
|
| gptkbp:manufacturer |
gptkb:Engine_Alliance
|
| gptkbp:numberOfStages |
2
9 |
| gptkbp:status |
in service
|
| gptkbp:thrust |
70,000–81,500 lbf
|
| gptkbp:usedOn |
gptkb:aircraft
|
| gptkbp:weight |
14,700 lb
|
| gptkbp:bfsParent |
gptkb:aircraft
|
| gptkbp:bfsLayer |
4
|