Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
0.76:1
|
| gptkbp:compressionRatio |
9-stage axial
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
46 in (1.17 m)
|
| gptkbp:family |
gptkb:General_Electric_F110
|
| gptkbp:firstFlight |
1984
|
| https://www.w3.org/2000/01/rdf-schema#label |
F110-GE-100
|
| gptkbp:length |
180 in (4.57 m)
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
28,200 lbf (afterburner)
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
gptkb:aircraft
F-14 Tomcat F-15E Strike Eagle |
| gptkbp:weight |
3,920 lb (1,780 kg)
|
| gptkbp:bfsParent |
gptkb:General_Electric_F110
|
| gptkbp:bfsLayer |
7
|