|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:F119-PW-600_Engine
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:YF-22
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:contract
|
gptkb:1991
|
|
gptkbp:controls
|
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
supercruise
|
|
gptkbp:developed_by
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:developer
|
$1 billion
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
twin-spool
|
|
gptkbp:engine_type
|
gptkb:3
2
|
|
gptkbp:environmental_impact
|
minimized
|
|
gptkbp:features
|
vectoring thrust
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:fuel_capacity
|
high
|
|
gptkbp:fuel_type
|
gptkb:JP-8
gptkb:full_authority_digital_engine_control_(FADEC)
annular combustor
|
|
gptkbp:has_programs
|
F135
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F119 program
|
|
gptkbp:integrates_with
|
gptkb:F-22_Raptor
|
|
gptkbp:is_tested_for
|
completed
|
|
gptkbp:key
|
stealth, speed, agility
|
|
gptkbp:legacy
|
advanced fighter engine technology
|
|
gptkbp:length
|
12 ft 4 in
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:max_speed
|
Mach 2.25
|
|
gptkbp:military_branch
|
gptkb:aircraft
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_status
|
gptkb:2005
|
|
gptkbp:partnerships
|
gptkb:Lockheed_Martin
|
|
gptkbp:power_output
|
30,000 shp
|
|
gptkbp:primary_user
|
gptkb:none
|
|
gptkbp:production_years
|
gptkb:1996
|
|
gptkbp:project
|
ongoing
|
|
gptkbp:propulsion
|
2.33
35,000 lbf
|
|
gptkbp:range
|
2,000 miles
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
65,000 ft
|
|
gptkbp:successor
|
gptkb:F135_engine
|
|
gptkbp:sustainability
|
high
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:F-22_Raptor
|
|
gptkbp:weight
|
1,500 lb
|