F401 (military derivative context)
E508850
The F401 is a military turbofan engine developed as a combat-optimized derivative of the Pratt & Whitney JT8D for use in fighter and attack aircraft.
Observed surface forms (1)
| Surface form | Occurrences |
|---|---|
| F401 | 0 |
Statements (24)
| Predicate | Object |
|---|---|
| instanceOf |
military aircraft engine
ⓘ
turbofan engine ⓘ |
| applicationStatus | intended for military use ⓘ |
| civilianBaseEngine | JT8D NERFINISHED ⓘ |
| configuration | turbofan core based on JT8D architecture ⓘ |
| countryOfOrigin |
United States of America
ⓘ
surface form:
United States
|
| derivedFrom | Pratt & Whitney JT8D NERFINISHED ⓘ |
| designedFor | fighter and attack aircraft ⓘ |
| designFeature | afterburning capability (intended) ⓘ |
| designLineage | civilian-to-military derivative ⓘ |
| designOptimization | combat performance ⓘ |
| developer | Pratt & Whitney NERFINISHED ⓘ |
| developmentGoal | provide a combat-optimized derivative of the JT8D ⓘ |
| engineType | low-bypass turbofan ⓘ |
| family | JT8D engine family NERFINISHED ⓘ |
| fuelType | jet fuel ⓘ |
| intendedRole |
attack aircraft engine
ⓘ
fighter aircraft engine ⓘ |
| manufacturer | Pratt & Whitney NERFINISHED ⓘ |
| marketSegment | military aviation ⓘ |
| natoName | F401 ⓘ |
| thrustClass | medium thrust ⓘ |
| useCase |
attack aircraft propulsion
ⓘ
fighter aircraft propulsion ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.