|
gptkbp:instance_of
|
gptkb:turbofan_engine
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Mc_Donnell_Douglas_F-15_E_Strike_Eagle
gptkb:F-15_K_Slam_Eagle
gptkb:F-15_EX
gptkb:F-4_G_Wild_Weasel
gptkb:F-15_C_Eagle
gptkb:F-15_D_Eagle
gptkb:F-15_SG
gptkb:F-15_SA
gptkb:F-15_E_Strike_Eagle
gptkb:F-4_E_Phantom_II
F-15 J Eagle
|
|
gptkbp:application
|
gptkb:military_aircraft
gptkb:fighter_aircraft
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
gptkb:3
gptkb:9
axial
|
|
gptkbp:control_system
|
gptkb:FADEC
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
gptkb:General_Electric
turbofan
|
|
gptkbp:design_features
|
high bypass ratio
|
|
gptkbp:development
|
gptkb:F101_engine_family
gptkb:General_Electric_F101
|
|
gptkbp:diameter
|
1.1 m
3.0 ft
|
|
gptkbp:elevation
|
up to 50,000 ft
|
|
gptkbp:emissions_standard
|
low
low emissions
|
|
gptkbp:engine
|
gptkb:F110-GE-100
gptkb:F119-PW-100
gptkb:General_Electric_F110
widely available
mass production
Brayton cycle
developed in the 1970s
air start
extensive support network
modernization programs
|
|
gptkbp:engine_configuration
|
twin-engine
twin-spool
pylon-mounted
detailed specifications available
dual-spool
F101-GE-102
|
|
gptkbp:engine_power
|
high reliability
3,000 hours
optimized for speed
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
turbofan
F101-GE-103
F101-GE-100
F101-GE-102 A
F101-GE-104
F101-GE-105
F101-GE-106
F101-GE-107
F101-GE-108
F101-GE-109
F101-GE-110
F101-GE-111
F101-GE-112
F101-GE-113
F101-GE-114
F101-GE-115
F101-GE-116
F101-GE-117
F101-GE-118
F101-GE-119
F101-GE-120
F101-GE-102 B
F101-GE-102 C
F101-GE-102 D
F101-GE-102 E
F101-GE-102 F
F101-GE-102 G
F101-GE-102 H
F101-GE-102 I
F101-GE-102 J
|
|
gptkbp:first_flight
|
gptkb:1972
|
|
gptkbp:first_introduced
|
gptkb:1972
gptkb:1976
|
|
gptkbp:fuel_capacity
|
1,200 kg
1.1 m
3.8 m
|
|
gptkbp:fuel_economy
|
high
0.8 lb/lbf/hr
0.85 lb/hp/hr
0.85 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
gptkb:Jet_A
electronic control
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric F101-GE-102
|
|
gptkbp:is_tested_for
|
ground testing
General Electric test facility
|
|
gptkbp:length
|
3.8 m
12.5 ft
|
|
gptkbp:maintenance
|
1,500 hours
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_speed
|
Mach 2.5
|
|
gptkbp:noise_level
|
low
low noise
|
|
gptkbp:notable_feature
|
variable area nozzle
|
|
gptkbp:notable_users
|
gptkb:United_States_Air_Force
|
|
gptkbp:number_of_stages
|
gptkb:9
|
|
gptkbp:number_of_turbine_stages
|
2
|
|
gptkbp:operational_range
|
2,000 miles
|
|
gptkbp:operational_use
|
gptkb:military_aircraft
gptkb:United_States_Air_Force
|
|
gptkbp:propulsion
|
0.24
29,000 lbf
25,000 lbf
9.67
23,500 lbf
29,000 lbf with afterburner
|
|
gptkbp:related_aircraft
|
gptkb:F-15
|
|
gptkbp:service_ceiling
|
65,000 ft
|
|
gptkbp:service_entry
|
gptkb:1976
|
|
gptkbp:turbine_type
|
2
axial
|
|
gptkbp:turbofan_family
|
gptkb:F101_family
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
gptkb:General_Dynamics_F-16_Fighting_Falcon
gptkb:Mc_Donnell_Douglas_F-15_Eagle
|
|
gptkbp:weight
|
1,200 kg
3,000 lb
|