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gptkbp:instance_of
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gptkb:engine
|
|
gptkbp:bfsLayer
|
6
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gptkbp:bfsParent
|
gptkb:GE_Aviation_Engineering
|
|
gptkbp:aircraft_operated
|
gptkb:star
air superiority
multirole fighter
|
|
gptkbp:average_temperature
|
1,600 ° C
|
|
gptkbp:cancellation_reason
|
gptkb:battle
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:combat_radius
|
1,839 km
|
|
gptkbp:compression_ratio
|
30:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
Pratt & Whitney engineers
|
|
gptkbp:developer
|
1990s
$1 billion
|
|
gptkbp:diameter
|
3.0 ft
|
|
gptkbp:emissions_standard
|
low emissions
variable geometry
|
|
gptkbp:engine
|
gptkb:aircraft
gptkb:F119_family
high performance
twin-engine
Brayton cycle
8,000 hours
air start
|
|
gptkbp:engine_type
|
gptkb:F119-PW-100
high bypass ratio
|
|
gptkbp:environmental_impact
|
gptkb:battle
|
|
gptkbp:features
|
modular design
vectoring thrust
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:fuel_capacity
|
high
0.5 lb/lbf/hr
1,360 kg
|
|
gptkbp:fuel_type
|
gptkb:JP-8
annular
dual fuel system
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F119-PW-9000 Engine
|
|
gptkbp:is_tested_for
|
static testing
Pratt & Whitney facility
|
|
gptkbp:length
|
16.5 ft
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:notable_feature
|
supercruise capability
|
|
gptkbp:operational_area
|
gptkb:aircraft
|
|
gptkbp:operational_range
|
1,200 nautical miles
|
|
gptkbp:power_output
|
27,000 lbf without afterburner
|
|
gptkbp:project
|
gptkb:F119_program
|
|
gptkbp:propulsion
|
gptkb:battle
5.0:1
35,000 lbf
|
|
gptkbp:rate_of_fire
|
high
|
|
gptkbp:safety_features
|
high
|
|
gptkbp:service_ceiling
|
65,000 ft
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Lockheed_Martin_F-22_Raptor
|
|
gptkbp:weight
|
3,000 lb
|