Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
0.30
|
| gptkbp:competitor |
gptkb:General_Electric_YF120
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:Advanced_Tactical_Fighter_program
|
| gptkbp:diameter |
1.17 m
|
| gptkbp:engineType |
afterburning turbofan
|
| gptkbp:firstFlight |
1990
|
| gptkbp:fuelType |
gptkb:JP-8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney YF119
|
| gptkbp:length |
4.9 m
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:status |
gptkb:prototype
not in production |
| gptkbp:successor |
gptkb:Pratt_&_Whitney_F119
|
| gptkbp:thrust |
35,000 lbf
|
| gptkbp:usedIn |
gptkb:YF-23
gptkb:YF-22 |
| gptkbp:weight |
1,700 kg
|
| gptkbp:bfsParent |
gptkb:Lockheed_YF-22
gptkb:Northrop_YF-23 gptkb:F-22_Raptor_prototype gptkb:YF-23 |
| gptkbp:bfsLayer |
7
|