|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:GE_Aviation_Operations
|
|
gptkbp:aircraft_operated
|
F-35 A, F-35 B, F-35 C
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
up to 1,600 ° C
|
|
gptkbp:certification
|
military certification
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:compression_ratio
|
30:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
|
gptkbp:cooling_system
|
air-cooled
water-based coolant
|
|
gptkbp:country
|
multiple NATO countries
|
|
gptkbp:design
|
8,000 hours
|
|
gptkbp:developer
|
$1 billion
|
|
gptkbp:diameter
|
3.0 ft
2.5 ft
|
|
gptkbp:drivetrain
|
integrated gearbox
|
|
gptkbp:emissions_standard
|
low
variable area intake
|
|
gptkbp:environmental_impact
|
reduced environmental impact
|
|
gptkbp:first_flight
|
gptkb:2006
|
|
gptkbp:fuel_capacity
|
high
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
annular combustor
high-pressure fuel pump
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F135-GE-100 engine
|
|
gptkbp:investment
|
high
|
|
gptkbp:is_designed_for
|
gptkb:star
|
|
gptkbp:is_tested_for
|
gptkb:NASA_Glenn_Research_Center
|
|
gptkbp:launch_date
|
30 seconds
|
|
gptkbp:length
|
16.5 ft
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_speed
|
Mach 1.6
|
|
gptkbp:noise_level
|
low
active vibration control system
|
|
gptkbp:notable_battle
|
combat-tested
|
|
gptkbp:operational_area
|
gptkb:2015
|
|
gptkbp:operational_status
|
multi-mode operation
|
|
gptkbp:part_of
|
gptkb:F-35_program
|
|
gptkbp:propulsion
|
gptkb:battle
29,000 lbf
|
|
gptkbp:research_and_development
|
ongoing R& D efforts
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:supply_chain
|
global supply chain
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:upgrades
|
planned upgrades
|
|
gptkbp:variant
|
gptkb:F135_engine_family
|
|
gptkbp:weight
|
3,000 lb
|