|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:air_support
|
high airflow
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:competes_with
|
gptkb:GE_F120
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
|
|
gptkbp:cooling_system
|
advanced cooling system
|
|
gptkbp:designed_for
|
gptkb:F-22_Raptor
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:diameter
|
3 ft 4 in
36 in
|
|
gptkbp:elevation
|
high altitude
|
|
gptkbp:emissions_standard
|
low emissions
|
|
gptkbp:engine
|
Brayton cycle
air start
|
|
gptkbp:engine_configuration
|
twin-engine
twin-engine configuration
|
|
gptkbp:engine_test
|
ground test
|
|
gptkbp:engine_type
|
military turbofan
|
|
gptkbp:fan_art
|
wide-chord fan
|
|
gptkbp:features
|
vectoring thrust
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:fuel_capacity
|
3 ft 4 in
1,500 lb
12 ft 4 in
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:JP-8
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F119-PW-107
|
|
gptkbp:length
|
12 ft 4 in
|
|
gptkbp:maintenance
|
low maintenance
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:military_technology
|
gptkb:United_States_Air_Force
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:operational_range
|
long operating range
|
|
gptkbp:operational_use
|
stealth missions
|
|
gptkbp:performance
|
superior performance
|
|
gptkbp:propulsion
|
yes
35,000 lbf
no thrust reverser
|
|
gptkbp:related_aircraft
|
fifth-generation fighter
|
|
gptkbp:related_to
|
gptkb:F-35_Lightning_II
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_entry
|
gptkb:2005
|
|
gptkbp:turbine_type
|
advanced alloys
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:video_output
|
dual-spool
|
|
gptkbp:weight
|
1,500 lb
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_F119
|
|
gptkbp:bfsLayer
|
5
|