Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
long-haul widebody aircraft
|
| gptkbp:bypassRatio |
8.7:1
|
| gptkbp:certification |
gptkb:FAA
2003 |
| gptkbp:compressionRatio |
23:1
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:family |
gptkb:GE90
|
| gptkbp:fanBladesMaterial |
composite titanium
|
| gptkbp:firstRun |
2001
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:hasConcept |
dual-spool
|
| gptkbp:length |
287 in
|
| gptkbp:mainRotorDiameter |
128 in
|
| gptkbp:manufacturer |
gptkb:GE_Aviation
|
| gptkbp:maximumSpeed |
115,300 lbf
|
| gptkbp:notableFor |
world's most powerful jet engine (as of 2024)
|
| gptkbp:relatedTo |
gptkb:GE9X
gptkb:GEnx |
| gptkbp:usedInAircraft |
gptkb:aircraft
gptkb:Boeing_777-200LR gptkb:Boeing_777F |
| gptkbp:weight |
19,316 lb
|
| gptkbp:bfsParent |
gptkb:General_Electric_GE90
gptkb:GE90_engine |
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
GE90-115B
|