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gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
6
|
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gptkbp:bfsParent
|
gptkb:GE_Aviation_Engineering
|
|
gptkbp:armament
|
blisk design
|
|
gptkbp:average_temperature
|
high temperature
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:combat_role
|
multirole fighter
|
|
gptkbp:commissioned
|
gptkb:2009
|
|
gptkbp:compression_ratio
|
30:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
stealth operations
|
|
gptkbp:developer
|
high development cost
|
|
gptkbp:diameter
|
3.0 ft
|
|
gptkbp:emissions_standard
|
low emissions
variable area
|
|
gptkbp:engine
|
8,000 hours
air start
pylon mounted
single spool
|
|
gptkbp:engine_type
|
gptkb:F135-PW-6000
high-pressure turbine
|
|
gptkbp:first_flight
|
gptkb:2006
|
|
gptkbp:fuel_capacity
|
high efficiency
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
annular combustor
|
|
gptkbp:global_presence
|
used by multiple countries
|
|
gptkbp:has_programs
|
gptkb:Joint_Strike_Fighter_(JSF)_program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F135-PW-3000 Engine
|
|
gptkbp:integrates_with
|
integrated with aircraft systems
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:length
|
16.5 ft
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:operational_range
|
1,380 nautical miles
|
|
gptkbp:operational_status
|
in service
|
|
gptkbp:partnerships
|
collaborative partnerships
|
|
gptkbp:performance
|
high performance
|
|
gptkbp:power_output
|
29,000 lbf without afterburner
|
|
gptkbp:propulsion
|
gptkb:battle
43,000 lbf
|
|
gptkbp:research_and_development
|
ongoing R& D efforts
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:sustainability
|
sustainable design
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:upgrades
|
planned upgrades
|
|
gptkbp:used_in
|
gptkb:star
|
|
gptkbp:weight
|
3,000 lb
|