Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:afterburning |
yes
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
0.30:1
|
| gptkbp:configuration |
axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
1.17 m
|
| gptkbp:features |
thrust vectoring nozzle
low observable design |
| gptkbp:firstFlight |
1997
|
| gptkbp:fuelType |
gptkb:JP-8
|
| https://www.w3.org/2000/01/rdf-schema#label |
F119 engine
|
| gptkbp:length |
4.87 m
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:militaryDesignation |
gptkb:PW1120
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:relatedTo |
gptkb:F135_engine
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
35,000 lbf
|
| gptkbp:usedIn |
F-22 Raptor
|
| gptkbp:weight |
1,700 kg
|
| gptkbp:bfsParent |
gptkb:Pratt_&_Whitney_Military_Engines
|
| gptkbp:bfsLayer |
7
|