|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:application
|
military aircraft
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:designatedAs
|
US_military_as_J79
|
|
gptkbp:diameter
|
30 in
|
|
gptkbp:engineConfiguration
|
turbojet
|
|
gptkbp:engineType
|
axial
single_spool
|
|
gptkbp:exhaustSystem
|
afterburning
variable geometry
|
|
gptkbp:firstFlight
|
1955
|
|
gptkbp:fuel_capacity
|
0.85 lb/hp/hr
|
|
gptkbp:fuelType
|
annular
spark plug
JP-4
hydromechanical
|
|
gptkbp:historicalEvent
|
developed in the 1950s
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
J79-GE-15
|
|
gptkbp:is_used_in
|
gptkb:McDonnell_Douglas_F-4_Phantom_II
|
|
gptkbp:length
|
14 ft 9 in
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:notable_feature
|
J79-GE-17
|
|
gptkbp:notableUsers
|
gptkb:Iranian_Air_Force
gptkb:Israeli_Air_Force
gptkb:Royal_Canadian_Air_Force
gptkb:United_States_Air_Force
gptkb:United_States_Navy
|
|
gptkbp:number_of_stages
|
8
|
|
gptkbp:operationalHistory
|
used in various military aircraft
|
|
gptkbp:operationalRange
|
0.5 to 2.0 Mach
|
|
gptkbp:propulsion
|
15,000 lbf
3.95
|
|
gptkbp:related_engine
|
gptkb:F110_engine
F119 engine
F119-PW-100 engine
F135 engine
F135-PW-100 engine
F404 engine
F119-PW-200 engine
F119-PW-300 engine
F135-PW-200 engine
F135-PW-300 engine
J85 engine
Brayton_cycle
|
|
gptkbp:replacedBy
|
F404 engine
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:type
|
turbojet engine
|
|
gptkbp:weight
|
3,800 lb
|