|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
F-5 family
|
|
gptkbp:application
|
military aircraft
|
|
gptkbp:climate
|
1,500 °F
|
|
gptkbp:controls
|
digital control
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:diameter
|
30 in
|
|
gptkbp:emissionsStandard
|
compliant with military standards
|
|
gptkbp:engineConfiguration
|
twin-shaft
|
|
gptkbp:engineType
|
axial
single_spool
|
|
gptkbp:exportedTo
|
various countries
|
|
gptkbp:firstFlight
|
1958
|
|
gptkbp:fuel_capacity
|
high
0.8 lb/hp/hr
|
|
gptkbp:fuelType
|
Jet A
annular
spark plug
|
|
gptkbp:hasDepartment
|
optional
|
|
gptkbp:historicalEvent
|
developed from J79 engine
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric J85-GE-5
|
|
gptkbp:is_used_in
|
gptkb:Northrop_F-5
|
|
gptkbp:legacy
|
widely used in military aviation.
|
|
gptkbp:length
|
12.5 in
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:notable_feature
|
J85-GE-13
|
|
gptkbp:number_of_stages
|
8
|
|
gptkbp:operational_status
|
training aircraft
|
|
gptkbp:operationalRange
|
1,000 miles
|
|
gptkbp:propulsion
|
7:1
3,850 lbf
|
|
gptkbp:related_engine
|
J85-GE-21
Brayton_cycle
|
|
gptkbp:reliability
|
high
|
|
gptkbp:retired
|
2000s
|
|
gptkbp:serviceHistory
|
used in various military applications
|
|
gptkbp:type
|
turbojet engine
|
|
gptkbp:weight
|
550 lb
|