|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:F-35_A
gptkb:F-35_B
gptkb:F-35_C
|
|
gptkbp:budget
|
$1.5 billion
|
|
gptkbp:bypass_ratio
|
5.0:1
|
|
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)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:designed_for
|
gptkb:Joint_Strike_Fighter
|
|
gptkbp:development
|
gptkb:General_Electric/_Rolls-Royce_F136
gptkb:General_Electric
|
|
gptkbp:diameter
|
3 ft 1 in
|
|
gptkbp:elevation
|
50,000 ft
|
|
gptkbp:emissions_standard
|
Nox standard
|
|
gptkbp:engine
|
gptkb:F119_family
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:engine_type
|
F136-1
F136-10
F136-2
F136-3
F136-4
F136-5
F136-6
F136-7
F136-8
F136-9
|
|
gptkbp:facilities
|
gptkb:NASA_Glenn_Research_Center
|
|
gptkbp:fan_art
|
wide-chord fan
|
|
gptkbp:first_flight
|
completed
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce F136
|
|
gptkbp:length
|
15 ft 8 in
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_use
|
gptkb:military
|
|
gptkbp:original_run
|
gptkb:2003
|
|
gptkbp:propulsion
|
29,000 lbf
|
|
gptkbp:status
|
cancelled
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:F-35_Lightning_II
|
|
gptkbp:weight
|
2,800 lb
|
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_Pegasus
gptkb:Pratt_&_Whitney_F135
|
|
gptkbp:bfsLayer
|
5
|