|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:General_Electric's_aviation_division
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:competes_with
|
gptkb:GE_F120_engine
|
|
gptkbp:contract
|
gptkb:2001
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
advanced thermal management
|
|
gptkbp:country
|
gptkb:Australia
gptkb:Italy
gptkb:Japan
gptkb:Monarch
gptkb:Netherlands
gptkb:Norway
gptkb:Politician
gptkb:United_Kingdom
gptkb:United_States
gptkb:Native_American_tribe
|
|
gptkbp:developer
|
$1.5 billion
|
|
gptkbp:diameter
|
3.0 ft
|
|
gptkbp:elevation
|
up to 50,000 ft
|
|
gptkbp:engine_type
|
high bypass ratio
two-stage turbine
|
|
gptkbp:features
|
stealth capabilities
|
|
gptkbp:first_flight
|
gptkb:2006
|
|
gptkbp:fuel_capacity
|
high fuel efficiency
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F135-PW-900 Engine
|
|
gptkbp:is_designed_for
|
gptkb:star
|
|
gptkbp:is_tested_for
|
completed in 2005
|
|
gptkbp:length
|
16.5 ft
|
|
gptkbp:maintenance
|
longer intervals
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:max_speed
|
Mach 1.6
|
|
gptkbp:noise_level
|
low noise emissions
|
|
gptkbp:operational_area
|
gptkb:2015
|
|
gptkbp:part_of
|
gptkb:F-35_program
|
|
gptkbp:performance
|
superior performance
|
|
gptkbp:propulsion
|
gptkb:battle
43,000 lbf
|
|
gptkbp:replaced_by
|
gptkb:F119-PW-100
|
|
gptkbp:sustainability
|
designed for reduced environmental impact
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:weight
|
3,000 lb
|