|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:air_support
|
high
|
|
gptkbp:aircraft_type
|
gptkb:stealth_technology
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:check_in_time
|
yes
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:competitors
|
gptkb:F120-PW-100
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
modular
|
|
gptkbp:development
|
1990s
|
|
gptkbp:diameter
|
1.2 m
|
|
gptkbp:emissions_standard
|
reduced
|
|
gptkbp:engine
|
gptkb:F119-PW-100
gptkb:significant
ongoing
cutting-edge technology
state-of-the-art technology
Brayton cycle
various military aircraft
air start
continuous improvements
promising.
high performance demands
|
|
gptkbp:engine_configuration
|
classified
advanced
twin-spool
pylon-mounted
|
|
gptkbp:engine_power
|
superior
|
|
gptkbp:features
|
vectoring thrust
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:fuel_economy
|
low
high
|
|
gptkbp:fuel_type
|
gptkb:JP-8
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F119-PW-106
|
|
gptkbp:is_tested_for
|
extensive
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
low
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:noise_level
|
low
reduced
|
|
gptkbp:operational_range
|
high altitude
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:propulsion
|
2.3
yes
high
35,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_entry
|
gptkb:2005
|
|
gptkbp:successor
|
gptkb:F135-PW-100
|
|
gptkbp:turbine_type
|
high bypass ratio
|
|
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
|