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gptkbp:instance_of
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gptkb:turbofan_engine
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gptkbp:application
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gptkb:military_aircraft
|
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gptkbp:certification
|
FAA certified
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|
gptkbp:combustor_type
|
annular
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gptkbp:compressor_type
|
axial
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gptkbp:control_system
|
hydromechanical
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gptkbp:cooling_system
|
air-cooled
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gptkbp:design
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gptkb:Pratt_&_Whitney
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gptkbp:diameter
|
3 ft 4 in
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|
gptkbp:elevation
|
up to 50,000 ft
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gptkbp:emissions_standard
|
NOx compliant
|
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gptkbp:engine
|
gptkb:Pratt_&_Whitney_F100
modular
Brayton cycle
air start
|
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gptkbp:engine_configuration
|
inline
twin-spool
|
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gptkbp:engine_type
|
FT8-1
FT8-10
FT8-11
FT8-12
FT8-13
FT8-14
FT8-15
FT8-16
FT8-17
FT8-18
FT8-19
FT8-2
FT8-20
FT8-3
FT8-4
FT8-5
FT8-6
FT8-7
FT8-8
FT8-9
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|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:fuel_economy
|
high efficiency
0.85 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney FT8
|
|
gptkbp:is_tested_for
|
ground testing
|
|
gptkbp:length
|
12 ft 6 in
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:max_speed
|
Mach 2.2
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:number_of_engines
|
two
|
|
gptkbp:operational_history
|
1960s to 1980s
|
|
gptkbp:propulsion
|
7.33
22,000 lbf
|
|
gptkbp:related_aircraft
|
F-4 Phantom II family
|
|
gptkbp:service
|
5,000 hours
|
|
gptkbp:successor
|
gptkb:Pratt_&_Whitney_F119
|
|
gptkbp:turbine_type
|
axial
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|
gptkbp:type
|
afterburning turbofan
|
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gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
|
|
gptkbp:weight
|
3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:General_Electric_LM2500
|
|
gptkbp:bfsLayer
|
8
|