Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
0.30:1
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
1.17 m
|
| gptkbp:features |
thrust vectoring nozzle
|
| gptkbp:firstFlight |
1997
|
| https://www.w3.org/2000/01/rdf-schema#label |
F119
|
| gptkbp:length |
3.81 m
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:relatedTo |
gptkb:F135
|
| gptkbp:status |
in production
|
| gptkbp:thrust |
35,000 lbf
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
F-22 Raptor
|
| gptkbp:weight |
1,700 kg
|
| gptkbp:bfsParent |
gptkb:Pratt_&_Whitney_jet_engines
gptkb:F135 gptkb:Oklahoma_City_Air_Logistics_Complex |
| gptkbp:bfsLayer |
7
|