|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:aircraft
|
gptkb:General_Dynamics_F-111
gptkb:F-111_family
|
|
gptkbp:controls
|
hydromechanical
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:developer
|
gptkb:United_States_Air_Force
|
|
gptkbp:diameter
|
3 ft 9 in
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
axial
|
|
gptkbp:fanBase
|
single-stage fan
|
|
gptkbp:firstFlight
|
1964
|
|
gptkbp:fuel_capacity
|
moderate
|
|
gptkbp:fuelType
|
annular
JP-4
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney TF30
|
|
gptkbp:is_used_in
|
gptkb:Grumman_F-111_Aardvark
gptkb:McDonnell_Douglas_F-4_Phantom_II
|
|
gptkbp:length
|
15 ft 6 in
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:maximum_speed
|
Mach_2.5
|
|
gptkbp:noise_level
|
yes
|
|
gptkbp:notable_feature
|
variable geometry
|
|
gptkbp:operationalRange
|
high subsonic to supersonic
up to 50,000 ft
|
|
gptkbp:productionYears
|
1960s
|
|
gptkbp:propulsion
|
22,000 lbf
5.79:1
|
|
gptkbp:related_engine
|
gptkb:Pratt_&_Whitney_F135-PW-400
gptkb:Pratt_&_Whitney_F135-PW-100
gptkb:Pratt_&_Whitney_F135
gptkb:Pratt_&_Whitney_F135-PW-600
Pratt & Whitney F119
Pratt & Whitney F119-PW-100
Pratt & Whitney F119-PW-400
Pratt & Whitney F119-PW-600
Brayton_cycle
|
|
gptkbp:retirementYear
|
1990s
|
|
gptkbp:serviceType
|
1967
|
|
gptkbp:successor
|
Pratt & Whitney F119
|
|
gptkbp:team
|
Pratt_&_Whitney_engineers
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:weight
|
3,800 lb
|