Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:Pratt_&_Whitney_F119
|
| gptkbp:aircraft_operated |
gptkb:aircraft
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypass_ratio |
5:1
|
| gptkbp:check_in_time |
gptkb:battle
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
1.2 m
1.1 m |
| gptkbp:engine |
dual-spool
|
| gptkbp:engine_type |
gptkb:3
2 |
| gptkbp:first_flight |
gptkb:1997
|
| gptkbp:fuel_type |
gptkb:JP-8
annular combustor |
| https://www.w3.org/2000/01/rdf-schema#label |
F119-PW-105
|
| gptkbp:length |
3.5 m
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:notable_features |
thrust vectoring
|
| gptkbp:propulsion |
35,000 lbf
|
| gptkbp:services |
gptkb:2005
|
| gptkbp:type |
gptkb:engine
|
| gptkbp:used_in |
gptkb:F-22_Raptor
|
| gptkbp:weight |
1,500 lb
|