General Electric F404-GE-102 turbofan
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
military jet aircraft
|
| gptkbp:bypassRatio |
0.34:1
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
3-stage fan, 7-stage axial compressor
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
35 in
|
| gptkbp:firstFlight |
1980s
|
| gptkbp:fuelType |
Jet-A, JP-5, JP-8
|
| gptkbp:hasTower |
1-stage high-pressure, 1-stage low-pressure
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric F404-GE-102 turbofan
|
| gptkbp:length |
154 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:part_of |
gptkb:General_Electric_F404_engine_family
|
| gptkbp:status |
in production
|
| gptkbp:thrust_(afterburner) |
19,000 lbf
|
| gptkbp:usedInAircraft |
gptkb:HAL_Tejas
|
| gptkbp:weight |
2,282 lb
|
| gptkbp:bfsParent |
gptkb:KAI_T-50_Golden_Eagle
gptkb:FA-50PH gptkb:FA-50 gptkb:T-50_Golden_Eagle |
| gptkbp:bfsLayer |
6
|