|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
8
|
|
gptkbp:bfsParent
|
gptkb:Mitsubishi_UH-60_J_Black_Hawk
|
|
gptkbp:application
|
gptkb:helicopter
|
|
gptkbp:average_temperature
|
up to 1,000 ° C
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:competitors
|
gptkb:Rolls-Royce_M250
|
|
gptkbp:compression_ratio
|
16:1
|
|
gptkbp:controls
|
digital control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
modular design
|
|
gptkbp:developer
|
ongoing development
|
|
gptkbp:diameter
|
approximately 14 in
|
|
gptkbp:drivetrain
|
integrated gearbox
|
|
gptkbp:emissions_standard
|
low emissions
|
|
gptkbp:engine_type
|
free turbine
|
|
gptkbp:first_flight
|
gptkb:1980s
|
|
gptkbp:fuel_capacity
|
high efficiency
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
gptkb:full_authority_digital_engine_control_(FADEC)
annular combustor
|
|
gptkbp:future_plans
|
future upgrades planned
|
|
gptkbp:historical_event
|
developed for military use
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
T700-GE-701 C engine
|
|
gptkbp:launched
|
starter-generator
|
|
gptkbp:legacy
|
widely used in military operations
|
|
gptkbp:length
|
approximately 40 in
|
|
gptkbp:maintenance
|
2,500 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:market
|
military aviation market
|
|
gptkbp:modifications
|
various modifications available
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:operational_range
|
wide operating range
|
|
gptkbp:partnerships
|
collaborations with military organizations
|
|
gptkbp:power_output
|
1,800 horsepower
|
|
gptkbp:propulsion
|
high power-to-weight ratio
1,800 shp
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
high altitude performance
|
|
gptkbp:successor
|
gptkb:T700-GE-701_D_engine
|
|
gptkbp:supports
|
extensive support network
|
|
gptkbp:training
|
pilot training available
|
|
gptkbp:type
|
turbo-shaft
|
|
gptkbp:used_in
|
gptkb:AH-64_Apache
gptkb:UH-60_Black_Hawk
|
|
gptkbp:weight
|
approximately 400 lb
|