|
gptkbp:instanceOf
|
turbo-shaft engine
|
|
gptkbp:application
|
military helicopters
|
|
gptkbp:certifications
|
FAA_certified
|
|
gptkbp:climate
|
up to 1,000 °C
|
|
gptkbp:compressionRatio
|
16:1
|
|
gptkbp:controls
|
digital electronic control
|
|
gptkbp:coolingSystem
|
air-cooled
oil-cooled
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:diameter
|
approximately 16 in
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissionsStandard
|
meets_EPA_standards
|
|
gptkbp:engine
|
low vibration
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
gptkb:T700-GE-701D
gptkb:T700-GE-701C
free turbine
axial compressor
T700-GE-701E
high turbine inlet temperature
T700-GE-701F
T700-GE-701G
T700-GE-701H
T700-GE-701I
T700-GE-701J
T700-GE-701K
T700-GE-701L
|
|
gptkbp:exhaustSystem
|
single exhaust
|
|
gptkbp:firstFlight
|
1980
|
|
gptkbp:fuel_capacity
|
high efficiency
approximately 0.5 lb/hp/hr
|
|
gptkbp:fuelType
|
gptkb:full_authority_digital_engine_control_(FADEC)
Jet A
annular
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
T700-GE-401C
|
|
gptkbp:is_used_in
|
gptkb:AH-64_Apache
gptkb:UH-60_Black_Hawk
|
|
gptkbp:launched
|
starter-generator
|
|
gptkbp:legal_principle
|
Brayton_cycle
|
|
gptkbp:length
|
approximately 48 in
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:market_segment
|
military aviation
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:number_of_stages
|
14 stages
|
|
gptkbp:operationalRange
|
up to 20,000 ft
|
|
gptkbp:powerOutput
|
1,500 to 2,000 shp
|
|
gptkbp:propulsion
|
1,800 shp
|
|
gptkbp:related_engine
|
T700 family
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:services
|
up to 5,000 hours
|
|
gptkbp:training
|
U.S._Army_program
|
|
gptkbp:type
|
turbo-shaft
|
|
gptkbp:weight
|
approximately 400 lb
|