|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:General_Electric's_aviation_division
|
|
gptkbp:aircraft_operated
|
gptkb:F-22_Raptor
air superiority
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:compression_ratio
|
30:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital
|
|
gptkbp:cooling_system
|
efficient
air-cooled
|
|
gptkbp:developer
|
1990s
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:emissions_standard
|
Nox standard compliant
|
|
gptkbp:engine
|
gptkb:aircraft
high
classified
ongoing
advanced
advanced materials
modular
twin-engine
state-of-the-art
superior
8,000 hours
air start
cutting-edge
dual-spool
|
|
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
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F119-PW-200 Engine
|
|
gptkbp:is_tested_for
|
ground testing
|
|
gptkbp:length
|
16 ft 6 in
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:max_speed
|
Mach 2.25
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_area
|
2005-present
|
|
gptkbp:operational_range
|
1,839 miles
|
|
gptkbp:propulsion
|
gptkb:battle
variable
11.67:1
35,000 lbf
|
|
gptkbp:service_ceiling
|
65,000 ft
|
|
gptkbp:technology
|
gptkb:aircraft
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Lockheed_Martin_F-22_Raptor
|
|
gptkbp:weight
|
3,000 lb
|