General Electric F414-GE-100
GPTKB entity
Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Boeing_F-15EX_Eagle_II
gptkb:KAI_KF-21_Boramae |
| gptkbp:bypassRatio |
0.94:1
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
7-stage axial compressor
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
35 inches
|
| gptkbp:family |
gptkb:General_Electric_F414
|
| gptkbp:firstFlight |
2010s
|
| gptkbp:fuelType |
Jet-A, JP-8
|
| gptkbp:hasTower |
1 high-pressure, 1 low-pressure
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric F414-GE-100
|
| gptkbp:length |
154 inches
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:status |
in production
|
| gptkbp:thrust |
22,000 lbf
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
gptkb:aircraft
|
| gptkbp:weight |
2,445 lb
|
| gptkbp:bfsParent |
gptkb:X-59_QueSST
|
| gptkbp:bfsLayer |
5
|