|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
advanced cooling system
|
|
gptkbp:design_purpose
|
air superiority
|
|
gptkbp:diameter
|
3.0 ft
2.5 ft
|
|
gptkbp:emissions_standard
|
EPA Tier 4
|
|
gptkbp:engine
|
gptkb:military_aircraft
gptkb:advanced_technology
gptkb:fighter_aircraft
modular design
mass production
Brayton cycle
ongoing development
periodic upgrades
air start
F118
F110
|
|
gptkbp:engine_configuration
|
inline
dual spool
detailed specifications
military rated
|
|
gptkbp:engine_materials
|
lightweight materials
|
|
gptkbp:engine_power
|
high reliability
high efficiency
high thrust-to-weight ratio
|
|
gptkbp:engine_type
|
F118-GE-101
|
|
gptkbp:first_flight
|
gptkb:1986
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:has_programs
|
gptkb:F119
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric F118-GE-100
|
|
gptkbp:is_tested_for
|
gptkb:NASA_Glenn_Research_Center
ground testing
|
|
gptkbp:length
|
12.5 ft
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_speed
|
Mach 2.5
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_range
|
2,400 miles
|
|
gptkbp:operational_use
|
gptkb:military
|
|
gptkbp:propulsion
|
no
29,000 lbf
|
|
gptkbp:related_aircraft
|
gptkb:F-15
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:turbine_type
|
high bypass ratio
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F-15_Eagle
|
|
gptkbp:weight
|
3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:B-2_Spirit
|
|
gptkbp:bfsLayer
|
4
|