Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:combustor_type |
annular
|
| gptkbp:compression_system |
dual-spool
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
3 ft 4 in
|
| gptkbp:features |
vectoring thrust
|
| gptkbp:first_flight |
gptkb:1997
|
| gptkbp:fuel_economy |
0.6 lb/hp/hr
|
| gptkbp:fuel_type |
gptkb:JP-8
|
| gptkbp:has_programs |
gptkb:Advanced_Tactical_Fighter
|
| https://www.w3.org/2000/01/rdf-schema#label |
F119-PW-109
|
| gptkbp:length |
12 ft 4 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:maximum_thrust_with_afterburner |
38,000 lbf
|
| gptkbp:propulsion |
35,000 lbf
|
| gptkbp:related_aircraft |
gptkb:F-22_family
|
| gptkbp:service_entry |
gptkb:2005
|
| gptkbp:turbine_type |
high-pressure and low-pressure turbines
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:used_in |
gptkb:F-22_Raptor
|
| gptkbp:weight |
1,800 lb
|
| gptkbp:bfsParent |
gptkb:Pratt_&_Whitney_F119
|
| gptkbp:bfsLayer |
5
|