Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:F119-PW-100_Engine
|
| gptkbp:aircraft_operated |
gptkb:F-22_family
|
| gptkbp:check_in_time |
gptkb:battle
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
3 ft 4 in
|
| gptkbp:engine_type |
axial
high bypass ratio |
| gptkbp:features |
vectoring thrust
|
| gptkbp:first_flight |
gptkb:1997
|
| gptkbp:fuel_capacity |
0.5 lb/lbf/hr
|
| gptkbp:fuel_type |
gptkb:JP-8
|
| https://www.w3.org/2000/01/rdf-schema#label |
F119-PW-100 A
|
| gptkbp:length |
16 ft 6 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:propulsion |
35,000 lbf
|
| gptkbp:service_ceiling |
65,000 ft
|
| gptkbp:type |
gptkb:engine
|
| gptkbp:used_in |
gptkb:F-22_Raptor
|
| gptkbp:weight |
3,000 lb
|