|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:F-35_A
gptkb:F-35_B
gptkb:F-35_C
|
|
gptkbp:cancellation_reason
|
yes
|
|
gptkbp:check_in_time
|
yes
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:competes_with
|
gptkb:Pratt_&_Whitney_F119
|
|
gptkbp:compressor_type
|
gptkb:3
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:designed_for
|
gptkb:Joint_Strike_Fighter
|
|
gptkbp:development
|
gptkb:2001
gptkb:Rolls-Royce
General Electric and Rolls-Royce
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:diameter
|
1.5 m
3.0 ft
|
|
gptkbp:elevation
|
up to 50,000 ft
|
|
gptkbp:emissions_standard
|
EPA Tier 4
|
|
gptkbp:engine
|
Brayton cycle
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:facilities
|
gptkb:NASA_Glenn_Research_Center
|
|
gptkbp:first_flight
|
gptkb:2006
|
|
gptkbp:fuel_economy
|
high
0.8 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:growth_rate
|
1,000 units
|
|
gptkbp:has_programs
|
JSF program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric F136
|
|
gptkbp:length
|
16.5 ft
|
|
gptkbp:lifespan
|
20 years
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:market_segment
|
gptkb:military_aircraft
|
|
gptkbp:notable_feature
|
variable area nozzle
|
|
gptkbp:operational_use
|
gptkb:military
|
|
gptkbp:original_run
|
gptkb:2003
|
|
gptkbp:projected_delivery
|
gptkb:2010
|
|
gptkbp:propulsion
|
optional
29,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:safety_rating
|
high
|
|
gptkbp:status
|
cancelled
|
|
gptkbp:test_engine
|
F136 engine test bed
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:F-35_Lightning_II
|
|
gptkbp:weight
|
3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:General_Electric_F101
|
|
gptkbp:bfsLayer
|
5
|