Pratt & Whitney F119-PW-100
GPTKB entity
Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:F-22_Raptor
gptkb:F-117_Nighthawk gptkb:Lockheed_Martin_F-22_Raptor gptkb:F22 |
| gptkbp:aircraft_operated |
gptkb:F-22_family
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:check_in_time |
gptkb:battle
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:developer |
1990s
|
| gptkbp:diameter |
1.2 m
|
| gptkbp:engine |
Brayton cycle
|
| gptkbp:engine_type |
gptkb:3
2 |
| gptkbp:fan_art |
dual rotor
|
| gptkbp:first_flight |
gptkb:1997
|
| gptkbp:fuel_type |
gptkb:Jet_A
annular |
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney F119-PW-100
|
| gptkbp:length |
3.5 m
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:notable_feature |
supercruise capability
|
| gptkbp:propulsion |
gptkb:battle
35,000 lbf |
| gptkbp:type |
gptkb:engine
|
| gptkbp:used_in |
gptkb:Lockheed_Martin_F-22_Raptor
|
| gptkbp:weight |
1,500 lb
|