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gptkbp:instance_of
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gptkb:engine
|
|
gptkbp:bfsLayer
|
4
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|
gptkbp:bfsParent
|
gptkb:General_Electric's_aviation_division
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
1,600 ° F
|
|
gptkbp:cancellation_reason
|
gptkb:battle
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:combat_radius
|
1,839 miles
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:developer
|
$1 billion
|
|
gptkbp:diameter
|
3.5 ft
|
|
gptkbp:emissions_standard
|
low emissions
variable geometry
|
|
gptkbp:engine
|
gptkb:F119_family
high reliability
twin-engine
Brayton cycle
superior performance
8,000 hours
35,000 lbf with afterburner
|
|
gptkbp:engine_type
|
gptkb:F119-PW-100_A
|
|
gptkbp:features
|
modular design
vectoring thrust
|
|
gptkbp:first_flight
|
gptkb:2005
|
|
gptkbp:fuel_capacity
|
high efficiency
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:JP-8
annular combustor
|
|
gptkbp:has_programs
|
gptkb:Joint_Advanced_Strike_Technology_(JAST)
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F119-PW-100 Engine
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:length
|
16.5 ft
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:max_speed
|
Mach 2.25
|
|
gptkbp:military_branch
|
gptkb:none
|
|
gptkbp:military_technology
|
air superiority
|
|
gptkbp:noise_level
|
low noise level
|
|
gptkbp:operational_area
|
gptkb:2005
|
|
gptkbp:original_run
|
gptkb:1996
|
|
gptkbp:propulsion
|
20 degrees
11.67:1
35,000 lbf
|
|
gptkbp:rate_of_fire
|
high
|
|
gptkbp:service_ceiling
|
65,000 ft
|
|
gptkbp:sustainability
|
sustainable design
|
|
gptkbp:technology
|
gptkb:aircraft
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:F-22_Raptor
|
|
gptkbp:weight
|
3,000 lb
|