|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:F-22_Raptor
gptkb:X-44_MANTA
F-35 Lightning II (proposed)
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:check_in_time
|
yes
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:commissioned
|
gptkb:2001
|
|
gptkbp:compressor_type
|
gptkb:3
|
|
gptkbp:control_system
|
digital electronic control
|
|
gptkbp:designed_for
|
gptkb:F-22_Raptor
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:diameter
|
1.2 m
|
|
gptkbp:engine
|
dual-spool
F119/ F120
|
|
gptkbp:engine_configuration
|
twin-engine
|
|
gptkbp:engine_type
|
gptkb:F119-PW-100
gptkb:F119-PW-101
gptkb:F119-PW-102
gptkb:F119-PW-103
gptkb:F119-PW-104
gptkb:F119-PW-105
gptkb:F119-PW-106
gptkb:F119-PW-107
gptkb:F119-PW-108
gptkb:F119-PW-109
|
|
gptkbp:features
|
vectoring thrust
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:JP-8
|
|
gptkbp:has_programs
|
Joint Advanced Strike Technology
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric F119
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
long
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operated_by
|
gptkb:United_States_Air_Force
gptkb:United_States_Navy
Japan Air Self-Defense Force (proposed)
Royal Air Force (proposed)
Singapore Air Force (proposed)
|
|
gptkbp:operational_use
|
gptkb:2005
|
|
gptkbp:propulsion
|
yes
35,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:weight
|
1,500 lb
|
|
gptkbp:bfsParent
|
gptkb:General_Electric_F101
|
|
gptkbp:bfsLayer
|
5
|