General Electric F110-GE-129
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
0.76:1
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
9-stage axial
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
46 in
|
| gptkbp:family |
gptkb:General_Electric_F110
|
| gptkbp:firstFlight |
1980s
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric F110-GE-129
|
| gptkbp:length |
180 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
29,000 lbf
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
gptkb:aircraft
F-15E Strike Eagle |
| gptkbp:weight |
3,920 lb
|
| gptkbp:bfsParent |
gptkb:F-15SG_Strike_Eagle
gptkb:KF-16 gptkb:Boeing_F-15SA gptkb:F-16_Block_70/72 |
| gptkbp:bfsLayer |
6
|