Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:Pratt_&_Whitney_F119
|
| gptkbp:aircraft_operated |
gptkb:F-22_family
|
| gptkbp:compression_ratio |
dual-spool
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
3 ft 4 in
|
| gptkbp:engine_type |
high-pressure and low-pressure turbines
|
| gptkbp:features |
vectoring thrust
|
| gptkbp:first_flight |
gptkb:1997
|
| gptkbp:fuel_capacity |
0.6 lb/hp/hr
|
| gptkbp:fuel_type |
gptkb:JP-8
annular |
| 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:propulsion |
38,000 lbf
35,000 lbf |
| gptkbp:services |
gptkb:2005
|
| gptkbp:type |
gptkb:engine
|
| gptkbp:used_in |
gptkb:F-22_Raptor
|
| gptkbp:weight |
1,800 lb
|