Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
2.0:1
|
| gptkbp:category |
gptkb:piston_engine
|
| gptkbp:compressionRatio |
9-stage axial
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
46 in
|
| gptkbp:family |
gptkb:General_Electric_F110
|
| gptkbp:firstFlight |
1980s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:hasTower |
2-stage high pressure, 2-stage low pressure
|
| gptkbp:length |
180 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:relatedTo |
gptkb:General_Electric_F110
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
19,000 lbf
|
| gptkbp:type |
non-afterburning turbofan
|
| gptkbp:usedIn |
gptkb:Lockheed_U-2S
gptkb:Northrop_Grumman_B-2_Spirit |
| gptkbp:weight |
3,920 lb
|
| gptkbp:bfsParent |
gptkb:General_Electric_F118-GE-100_turbofan
gptkb:U-2_spy_plane |
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
General Electric F118
|