General Electric F404-GE-102
GPTKB entity
Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
0.34:1
|
| gptkbp:combustorType |
annular
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
35 inches
|
| gptkbp:family |
gptkb:General_Electric_F404
|
| gptkbp:firstFlight |
1980s
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric F404-GE-102
|
| gptkbp:length |
154 inches
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:numberOfStages |
3 fan, 7 axial HP
1 HP, 1 LP |
| gptkbp:relatedTo |
gptkb:General_Electric_F414
gptkb:General_Electric_F404-GE-400 |
| gptkbp:status |
in production
|
| gptkbp:thrust |
19,000 lbf
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
gptkb:HAL_Tejas
|
| gptkbp:weight |
2,282 lb
|
| gptkbp:bfsParent |
gptkb:Hürjet_advanced_jet_trainer
|
| gptkbp:bfsLayer |
8
|