|
gptkbp:instanceOf
|
turbojet engine
|
|
gptkbp:application
|
military helicopters
civil helicopters
|
|
gptkbp:climate
|
high
|
|
gptkbp:compressionRatio
|
10:1
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
1960s
|
|
gptkbp:design_feature
|
advanced aerodynamics
lightweight materials
modular design
high thrust-to-weight ratio
digital control systems
|
|
gptkbp:developer
|
gptkb:General_Electric_Company
|
|
gptkbp:diameter
|
14 in
|
|
gptkbp:emissionsStandard
|
low
|
|
gptkbp:engineConfiguration
|
single_spool
|
|
gptkbp:engineType
|
free turbine
|
|
gptkbp:firstFlight
|
1959
|
|
gptkbp:fuel_capacity
|
high
|
|
gptkbp:fuelType
|
Jet A
annular
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric T64
|
|
gptkbp:is_used_in
|
gptkb:Lockheed_P-3_Orion
Bell UH-1 Iroquois
|
|
gptkbp:length
|
40 in
|
|
gptkbp:maintenance
|
moderate
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:notable_feature
|
T64-GE-416
T64-GE-419
T64-GE-420
T64-GE-421
T64-GE-425
|
|
gptkbp:operationalHistory
|
used in various military applications
|
|
gptkbp:powerOutput
|
1,000 shp
|
|
gptkbp:propulsion
|
1,500 lbf
|
|
gptkbp:related_engine
|
gptkb:General_Electric_T408
gptkb:Turbomeca_Arriel
gptkb:General_Electric_T64-GE-421
gptkb:General_Electric_T64-GE-420
gptkb:Honeywell_T53
gptkb:Pratt_&_Whitney_PT6
gptkb:General_Electric_T64-GE-419
gptkb:General_Electric_T700
gptkb:General_Electric_T58
gptkb:General_Electric_T64-GE-425
gptkb:Rolls-Royce_M250
gptkb:Turbomeca_TM319
T64 family
Brayton_cycle
|
|
gptkbp:reliability
|
high
|
|
gptkbp:services
|
long
|
|
gptkbp:successor
|
gptkb:General_Electric_T700
|
|
gptkbp:type
|
turbo-shaft engine
|
|
gptkbp:weight
|
300 lb
|