General Electric F404-GE-400
GPTKB entity
Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:McDonnell_Douglas_F/A-18_Hornet
gptkb:Northrop_F-20_Tigershark gptkb:Dassault_Rafale_(early_prototypes) |
| gptkbp:bypassRatio |
0.34:1
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
7-stage axial
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
35 in
|
| gptkbp:family |
gptkb:General_Electric_F404
|
| gptkbp:firstFlight |
1978
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric F404-GE-400
|
| gptkbp:length |
154 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
17,700 lbf
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
F/A-18 Hornet
|
| gptkbp:weight |
2,282 lb
|
| gptkbp:bfsParent |
gptkb:Douglas_X-31
|
| gptkbp:bfsLayer |
6
|