|
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
|
1,600 ° F
|
|
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:developer
|
$1.5 billion
|
|
gptkbp:diameter
|
3.0 ft
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
air start
turbojet cycle
|
|
gptkbp:first_flight
|
gptkb:2006
|
|
gptkbp:fuel_capacity
|
high
|
|
gptkbp:fuel_type
|
gptkb:JP-8
annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F135-PW-7000 Engine
|
|
gptkbp:investment
|
high pressure
|
|
gptkbp:is_designed_for
|
gptkb:star
|
|
gptkbp:length
|
16.5 ft
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:max_speed
|
Mach 1.6
|
|
gptkbp:military_branch
|
gptkb:aircraft
gptkb:battle
|
|
gptkbp:military_technology
|
gptkb:battle
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:produced_by
|
over 1,000
|
|
gptkbp:production_years
|
gptkb:2009
|
|
gptkbp:propulsion
|
gptkb:battle
43,000 lbf
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:technology
|
gptkb:aircraft
network-centric warfare
advanced avionics
sensor fusion
supercruise capability
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:variant
|
gptkb:F135-PW-6000
|
|
gptkbp:weight
|
3,000 lb
|