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gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:GE_Aviation_Engineering
|
|
gptkbp:aircraft_operated
|
gptkb:star
|
|
gptkbp:bypass_ratio
|
5:1
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:compression_ratio
|
30:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
3.0 ft
3.5 ft
|
|
gptkbp:emissions_standard
|
Nox standard compliant
|
|
gptkbp:engine
|
gptkb:aircraft
gptkb:advanced_technology
modular design
high reliability
ongoing upgrades
Brayton cycle
high efficiency
twin-spool
global support network
supercruise capability
continuous innovation
long lifecycle
|
|
gptkbp:engine_type
|
gptkb:F119-PW-100
turbofan
high-pressure turbine
|
|
gptkbp:fan_art
|
wide-chord fan
|
|
gptkbp:features
|
vectoring thrust
|
|
gptkbp:first_flight
|
gptkb:2005
|
|
gptkbp:fuel_capacity
|
3.5 ft
1,500 lb
0.5 lb/lbf/hr
16.5 ft
|
|
gptkbp:fuel_type
|
gptkb:JP-8
annular combustor
electronic fuel control
|
|
gptkbp:has_programs
|
gptkb:Joint_Strike_Fighter
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F119-PW-8000 Engine
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:length
|
16.5 ft
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:operational_range
|
1,839 miles
|
|
gptkbp:original_run
|
gptkb:1996
|
|
gptkbp:propulsion
|
gptkb:battle
23:1
35,000 lbf
|
|
gptkbp:service_ceiling
|
65,000 ft
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:F-22_Raptor
|
|
gptkbp:weight
|
1,500 lb
|