General Electric F404-GE-IN20
GPTKB entity
Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:afterburning |
yes
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
0.34:1
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
0.89 m
|
| gptkbp:family |
gptkb:General_Electric_F404
|
| gptkbp:firstFlight |
1980s (F404 family)
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric F404-GE-IN20
|
| gptkbp:intendedUse |
gptkb:Indian_Air_Force
|
| gptkbp:length |
3.91 m
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:numberOfStages |
3 fan, 7 axial HP
|
| gptkbp:thrust |
84 kN
|
| gptkbp:usedIn |
gptkb:HAL_Tejas
|
| gptkbp:weight |
1,035 kg
|
| gptkbp:bfsParent |
gptkb:Tejas_aircraft
gptkb:HAL_Tejas |
| gptkbp:bfsLayer |
6
|