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gptkbp:instance_of
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gptkb:engine
|
|
gptkbp:bfsLayer
|
4
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|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_F100
|
|
gptkbp:aircraft_operated
|
gptkb:F-111_family
gptkb:F-111_A
gptkb:F-111_B
gptkb:F-111_C
gptkb:F-111_D
gptkb:F-111_E
gptkb:F-111_F
gptkb:F-111_G
gptkb:F-111_H
gptkb:F-111_K
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|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:designated_as
|
gptkb:aircraft
|
|
gptkbp:developer
|
gptkb:F119_engine
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:engine
|
gptkb:General_Electric_F110
gptkb:Pratt_&_Whitney_F135
gptkb:Pratt_&_Whitney_F119
Brayton cycle
twin-spool
pylon-mounted
Rolls-Royce R B211
|
|
gptkbp:engine_type
|
axial compressor
high bypass ratio turbine
|
|
gptkbp:fan_art
|
single-stage fan
|
|
gptkbp:first_flight
|
gptkb:1967
|
|
gptkbp:fuel_capacity
|
0.8 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
annular combustion chamber
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney F101
|
|
gptkbp:length
|
12 ft 6 in
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:notable_features
|
variable area nozzle
|
|
gptkbp:number_of_stages
|
8 stages
|
|
gptkbp:operational_area
|
gptkb:aircraft
gptkb:Israeli_Air_Force
gptkb:Royal_Saudi_Air_Force
gptkb:military_base
gptkb:battle
|
|
gptkbp:propulsion
|
25,000 lbf
|
|
gptkbp:retirement_year
|
2000s
|
|
gptkbp:services
|
gptkb:1970
|
|
gptkbp:successor
|
gptkb:Pratt_&_Whitney_F135
gptkb:Pratt_&_Whitney_F119
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:used_in
|
gptkb:General_Dynamics_F-111_Aardvark
gptkb:Mc_Donnell_Douglas_F-15_Eagle
|
|
gptkbp:weight
|
3,000 lb
|