Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
variable
|
| gptkbp:competitor |
gptkb:Pratt_&_Whitney_YF119
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:Advanced_Tactical_Fighter_program
|
| gptkbp:firstFlight |
1990
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric YF120
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:notableFeature |
variable cycle technology
|
| gptkbp:program_outcome |
not selected for production
|
| gptkbp:status |
gptkb:prototype
|
| gptkbp:thrust_with_afterburner |
35,000 lbf
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:used_in |
gptkb:YF-23
gptkb:YF-22 |
| gptkbp:bfsParent |
gptkb:Lockheed_YF-22
gptkb:Northrop_YF-23 gptkb:F-22_Raptor_prototype gptkb:YF-23 |
| gptkbp:bfsLayer |
7
|