Statements (32)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
46 inches
|
| gptkbp:firstFlight |
2000
|
| gptkbp:fuelType |
gptkb:JP-4
gptkb:JP-8 JP-5 |
| gptkbp:intendedAircraft |
gptkb:Joint_Strike_Fighter
|
| gptkbp:length |
220 inches
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:notableFeature |
designed for stealth
capable of short takeoff and vertical landing (STOVL) in F-35B |
| gptkbp:predecessor |
gptkb:F119_engine
|
| gptkbp:primaryUser |
gptkb:Lockheed_Martin
|
| gptkbp:programStart |
1996
|
| gptkbp:relatedTo |
gptkb:F119_engine
|
| gptkbp:status |
in production
|
| gptkbp:thrust |
28,000 lbf (dry)
43,000 lbf (with afterburner) |
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
gptkb:F-35A
gptkb:F-35B gptkb:F-35C F-35 Lightning II |
| gptkbp:variant |
gptkb:F135-PW-100
gptkb:F135-PW-400 gptkb:F135-PW-600 |
| gptkbp:weight |
3,750 lb
|
| gptkbp:bfsParent |
gptkb:RTX_Corporation
gptkb:Pratt_&_Whitney_Military_Engines |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
F135 engine
|