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gptkbp:instance_of
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gptkb:engine
|
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gptkbp:bfsLayer
|
3
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gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:aircraft_operated
|
gptkb:F-35_A
gptkb:F-35_B
gptkb:F-35_C
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:armament
|
blisk design
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:compression_ratio
|
30:1
|
|
gptkbp:controls
|
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:country
|
gptkb:horse_race
gptkb:Australia
gptkb:Italy
gptkb:Japan
gptkb:Monarch
gptkb:Netherlands
gptkb:Norway
gptkb:Politician
gptkb:United_Kingdom
gptkb:United_States
|
|
gptkbp:design
|
modular design
|
|
gptkbp:developer
|
$1 billion
|
|
gptkbp:diameter
|
1.2 m
|
|
gptkbp:drivetrain
|
integrated gearbox
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
Brayton cycle
|
|
gptkbp:facilities
|
gptkb:NASA_Glenn_Research_Center
|
|
gptkbp:first_flight
|
gptkb:2006
|
|
gptkbp:fuel_capacity
|
high
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F135-PW-100
|
|
gptkbp:is_designed_for
|
gptkb:star
|
|
gptkbp:launch_date
|
30 seconds
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:max_speed
|
Mach 1.6
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_area
|
gptkb:military_unit
high-altitude
|
|
gptkbp:operational_range
|
1,380 miles
|
|
gptkbp:partnership
|
gptkb:Lockheed_Martin
|
|
gptkbp:propulsion
|
gptkb:battle
43,000 lbf
|
|
gptkbp:research_and_development
|
ongoing
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:successor
|
gptkb:F119-PW-100
|
|
gptkbp:supports
|
global support network
|
|
gptkbp:sustainability
|
designed for long life
|
|
gptkbp:technology
|
adaptive cycle engine
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:weight
|
1,500 kg
|