|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:GE_Aviation_Engineering
|
|
gptkbp:application
|
multirole stealth fighter
|
|
gptkbp:armament
|
blisk design
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:certification
|
gptkb:military_unit
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:compression_ratio
|
30:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
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:design
|
8,000 hours
|
|
gptkbp:developer
|
$1.5 billion
|
|
gptkbp:diameter
|
3.0 ft
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
high cycle
|
|
gptkbp:first_flight
|
gptkb:2006
|
|
gptkbp:fuel_capacity
|
high
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F135-PW-9000 Engine
|
|
gptkbp:integrates_with
|
gptkb:aircraft
|
|
gptkbp:investment
|
high
|
|
gptkbp:is_designed_for
|
gptkb:star
|
|
gptkbp:is_tested_for
|
extensive
|
|
gptkbp:launch_date
|
short
|
|
gptkbp:length
|
16.5 ft
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_range
|
1,380 nautical miles
|
|
gptkbp:production_years
|
gptkb:2009
|
|
gptkbp:propulsion
|
gptkb:battle
43,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:supports
|
global supply chain
|
|
gptkbp:sustainability
|
high
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:weight
|
3,000 lb
|