General Electric F404-GE-100D
GPTKB entity
Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:trainer_aircraft
|
| gptkbp:bypassRatio |
0.34:1
|
| gptkbp:compressionRatio |
25:1
|
| gptkbp:configuration |
afterburning turbofan
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
35 inches
|
| gptkbp:family |
gptkb:General_Electric_F404
|
| gptkbp:firstFlight |
early 2000s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric F404-GE-100D
|
| gptkbp:length |
154 inches
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:status |
in production
|
| gptkbp:thrust |
17,700 lbf
|
| gptkbp:usedInAircraft |
gptkb:KAI_T-50_Golden_Eagle
|
| gptkbp:weight |
2,282 lb
|
| gptkbp:bfsParent |
gptkb:A-4SU_Super_Skyhawk
|
| gptkbp:bfsLayer |
7
|