|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_F119
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:competitors
|
gptkb:F120-PW-100
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
modular
|
|
gptkbp:developer
|
1990s
|
|
gptkbp:diameter
|
1.2 m
|
|
gptkbp:emissions_standard
|
reduced
|
|
gptkbp:engine
|
gptkb:F119-PW-100
gptkb:significant
classified
ongoing
advanced
cutting-edge technology
state-of-the-art technology
Brayton cycle
twin-spool
superior
various military aircraft
air start
pylon-mounted
continuous improvements
promising.
high performance demands
|
|
gptkbp:engine_type
|
axial
high bypass ratio
|
|
gptkbp:features
|
vectoring thrust
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:fuel_capacity
|
low
high
|
|
gptkbp:fuel_type
|
gptkb:JP-8
annular
|
|
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
|
gptkb:battle
2.3
high
35,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:services
|
gptkb:2005
|
|
gptkbp:successor
|
gptkb:F135-PW-100
|
|
gptkbp:supports
|
high
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:F-22_Raptor
|
|
gptkbp:weight
|
1,500 lb
|