F119-PW-105

URI: https://gptkb.org/entity/F119-PW-105
GPTKB entity
Statements (25)
Predicate Object
gptkbp:instance_of gptkb:jet_engine
gptkbp:application gptkb:military_aircraft
gptkbp:bypass_ratio 5:1
gptkbp:check_in_time yes
gptkbp:combustor_type annular combustor
gptkbp:compressor_type gptkb:3
gptkbp:control_system gptkb:full_authority_digital_engine_control_(FADEC)
gptkbp:diameter 1.2 m
1.1 m
gptkbp:engine dual-spool
gptkbp:first_flight gptkb:1997
gptkbp:fuel_type gptkb:JP-8
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:related_aircraft gptkb:stealth_technology
gptkbp:service_entry gptkb:2005
gptkbp:turbine_type 2
gptkbp:type gptkb:turbofan_engine
gptkbp:used_in gptkb:F-22_Raptor
gptkbp:weight 1,500 lb
gptkbp:bfsParent gptkb:Pratt_&_Whitney_F119
gptkbp:bfsLayer 5