General Electric F118-GE-100
GPTKB entity
Statements (20)
Predicate | Object |
---|---|
gptkbp:instanceOf |
piston engine
|
gptkbp:application |
gptkb:aircraft
|
gptkbp:bypassRatio |
2.0:1
|
gptkbp:compressionRatio |
3-stage fan, 9-stage high-pressure compressor
|
gptkbp:countryOfOrigin |
gptkb:United_States
|
gptkbp:diameter |
46 in
|
gptkbp:family |
gptkb:General_Electric_F110
|
gptkbp:firstFlight |
1989
|
gptkbp:hasTower |
2-stage high-pressure, 2-stage low-pressure
|
https://www.w3.org/2000/01/rdf-schema#label |
General Electric F118-GE-100
|
gptkbp:length |
180 in
|
gptkbp:manufacturer |
gptkb:General_Electric
|
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:4_×_General_Electric_F118-GE-100_turbofans
|
gptkbp:bfsLayer |
7
|