|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:airlines
|
high airflow
|
|
gptkbp:application
|
gptkb:Sikorsky_CH-53K_King_Stallion
gptkb:Sikorsky_UH-60_Black_Hawk
gptkb:Bell_Boeing_V-22_Osprey
|
|
gptkbp:certifications
|
FAA_certified
|
|
gptkbp:climate
|
high temperature
|
|
gptkbp:competitors
|
gptkb:Honeywell_T53
gptkb:Pratt_&_Whitney_Canada_PT6
gptkb:Rolls-Royce_AE_1107C
|
|
gptkbp:compressionRatio
|
16:1
5:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
twin-spool
|
|
gptkbp:developer
|
CT7-2
CT7-8
CT7-9B
|
|
gptkbp:diameter
|
1.5 m
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissionsStandard
|
low emissions
|
|
gptkbp:engineConfiguration
|
twin-engine
|
|
gptkbp:engineType
|
high-pressure turbine
low-pressure turbine
single shaft
|
|
gptkbp:firstFlight
|
1970
|
|
gptkbp:fuel_capacity
|
high fuel efficiency
|
|
gptkbp:fuelType
|
Jet A
annular
|
|
gptkbp:height
|
1.2 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric CT7
|
|
gptkbp:is_used_in
|
military aircraft
|
|
gptkbp:launched
|
electric starter
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
3,600 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:market
|
military and commercial aviation
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notableUsers
|
gptkb:U.S._Army
gptkb:U.S._Navy
gptkb:U.S._Air_Force
international military forces
|
|
gptkbp:operationalRange
|
long operational range
|
|
gptkbp:powerOutput
|
5,000 to 7,000 shp
|
|
gptkbp:productionYears
|
1960s to 1970s
|
|
gptkbp:propulsion
|
up to 7,000 lbf
|
|
gptkbp:related_engine
|
CT7 family
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:successor
|
gptkb:General_Electric_GE38
|
|
gptkbp:weight
|
approximately 1,500 lb
|