General Electric F414-GE-100 turbofan
GPTKB entity
Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
0.94:1
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
7-stage axial HP, 3-stage axial LP
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
35 in
|
| gptkbp:family |
gptkb:General_Electric_F414
|
| gptkbp:firstFlight |
2015
|
| gptkbp:hasTower |
1-stage HP, 1-stage LP
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric F414-GE-100 turbofan
|
| gptkbp:length |
154 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:status |
in production
|
| gptkbp:thrust |
yes
22,000 lbf |
| gptkbp:usedIn |
gptkb:KAI_KF-21_Boramae
|
| gptkbp:weight |
2,445 lb
|
| gptkbp:bfsParent |
gptkb:Low-Boom_Flight_Demonstrator
|
| gptkbp:bfsLayer |
6
|