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gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_F117-PW-100
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:F-22_Raptor
|
|
gptkbp:budget
|
$10 million per unit
|
|
gptkbp:cancellation_reason
|
gptkb:battle
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:combat_radius
|
1,839 km
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
advanced cooling techniques
|
|
gptkbp:developer
|
1990s
$1 billion
|
|
gptkbp:diameter
|
1.2 m
|
|
gptkbp:elevation
|
up to 65,000 ft
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
gptkb:aircraft
high
classified
ongoing
advanced materials
twin-engine
6,000 hours
high bypass ratio
collaborative effort
superior to predecessors
|
|
gptkbp:engine_type
|
gptkb:none
gptkb:3
2
dual-spool
|
|
gptkbp:features
|
variable cycle
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:flows_into
|
integrated
|
|
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 series
|
|
gptkbp:is_designed_for
|
gptkb:F-22_Raptor
|
|
gptkbp:is_tested_for
|
extensive
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:max_speed
|
Mach 2.25
|
|
gptkbp:operational_area
|
gptkb:2005
|
|
gptkbp:propulsion
|
gptkb:battle
24:1
enhances maneuverability
35,000 lbf
27,000 lbf without afterburner
35,000 lbf with afterburner
|
|
gptkbp:rating
|
excellent
|
|
gptkbp:service_ceiling
|
65,000 ft
|
|
gptkbp:successor
|
gptkb:F135_engine
|
|
gptkbp:technology
|
gptkb:aircraft
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:F-22_Raptor
|
|
gptkbp:weight
|
1,500 lb
|