Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:F-35A
gptkb:F-35C |
| gptkbp:bypassRatio |
0.57:1
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
46 in (1.17 m)
|
| gptkbp:family |
gptkb:F135_engine_family
|
| gptkbp:firstFlight |
2006
|
| gptkbp:fuelType |
gptkb:JP-8
|
| gptkbp:hasConcept |
derived from F119 core
|
| https://www.w3.org/2000/01/rdf-schema#label |
F135-PW-400
|
| gptkbp:intendedUse |
gptkb:conventional_takeoff_and_landing_(CTOL)
carrier-based operations (CV) |
| gptkbp:length |
220 in (5.6 m)
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:relatedTo |
gptkb:F119_engine
|
| gptkbp:status |
in production
|
| gptkbp:thrust |
yes
28,000 lbf (dry) 43,000 lbf (with afterburner) |
| gptkbp:usedBy |
gptkb:United_States_Air_Force
gptkb:United_States_Navy international F-35 operators |
| gptkbp:usedIn |
F-35 Lightning II
|
| gptkbp:weight |
3,750 lb (1,700 kg)
|
| gptkbp:bfsParent |
gptkb:F135
gptkb:Pratt_&_Whitney_F135_engine |
| gptkbp:bfsLayer |
7
|