|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_F119
|
|
gptkbp:aircraft_operated
|
gptkb:F-22_family
gptkb:star
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:combat_role
|
air superiority
|
|
gptkbp:compression_ratio
|
30:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
advanced cooling techniques
|
|
gptkbp:design
|
modular design
|
|
gptkbp:developer
|
1990s
|
|
gptkbp:diameter
|
3 ft 4 in
44 in
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
gptkb:F119
gptkb:advanced_technology
advanced materials
Brayton cycle
twin-spool
superior
stealth missions
8,000 hours
|
|
gptkbp:engine_type
|
gptkb:F119-PW-100
high-pressure turbine
|
|
gptkbp:fan_art
|
wide-chord fan
|
|
gptkbp:features
|
vectoring thrust
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:fuel_capacity
|
high
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:JP-8
annular combustor
|
|
gptkbp:has_programs
|
gptkb:Joint_Strike_Fighter_program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F119-PW-104
|
|
gptkbp:is_tested_for
|
extensive
|
|
gptkbp:length
|
16 ft 6 in
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_area
|
gptkb:aircraft
gptkb:2005
|
|
gptkbp:propulsion
|
gptkb:battle
high
with afterburner
without afterburner
35,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
65,000 ft
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:F-22_Raptor
|
|
gptkbp:weight
|
3,000 lb
|