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gptkbp:instance_of
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gptkb:engine
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:GE_Aviation_Operations
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
1,600 ° F
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:compression_ratio
|
24:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital
|
|
gptkbp:cooling_system
|
air-cooled
interstage cooling
|
|
gptkbp:design
|
high bypass ratio
|
|
gptkbp:developer
|
derived from F110 engine
|
|
gptkbp:diameter
|
1.1 m
|
|
gptkbp:elevation
|
up to 50,000 ft
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
gptkb:F110_family
high performance
twin-engine
twin-spool
air start
pylon-mounted
up to 10,000 hours
|
|
gptkbp:engine_type
|
high-pressure turbine
military turbofan
|
|
gptkbp:fan_art
|
wide-chord fan
|
|
gptkbp:first_flight
|
gptkb:1981
|
|
gptkbp:fuel_capacity
|
high
1.1 m
3.8 m
680 kg
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
annular
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F118 engine
|
|
gptkbp:is_tested_for
|
static and flight testing
|
|
gptkbp:launch_date
|
30 seconds
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_speed
|
16,000 lbf
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_area
|
stealth operations
|
|
gptkbp:propulsion
|
gptkb:battle
10:1
14,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:services
|
gptkb:1983
|
|
gptkbp:supports
|
2,000 lb/s
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Lockheed_Martin_F-117_Nighthawk
|
|
gptkbp:water_source
|
1,200 lb/hr
|
|
gptkbp:weight
|
1,500 lb
|