|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:helicopter
|
|
gptkbp:average_temperature
|
up to 1,000 ° C
|
|
gptkbp:certification
|
EASA certified
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_stage
|
8 stages
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
digital control system
FADEC system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
modular design
|
|
gptkbp:development
|
1980s to 1990s
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine_configuration
|
twin-shaft
|
|
gptkbp:engine_type
|
MTR390-2
MTR390-3
MTR390-4
MTR390-5
|
|
gptkbp:first_flight
|
gptkb:1990
|
|
gptkbp:fuel_capacity
|
1,200 mm
600 mm
|
|
gptkbp:fuel_economy
|
high efficiency
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Turbomeca MTR390
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Safran_Helicopter_Engines
|
|
gptkbp:market_segment
|
gptkb:military_aircraft
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:operational_range
|
varies by application
|
|
gptkbp:operational_use
|
combat missions
|
|
gptkbp:partnership
|
gptkb:Leonardo_S.p._A.
gptkb:Lockheed_Martin
gptkb:Northrop_Grumman
gptkb:General_Dynamics
gptkb:Rafael_Advanced_Defense_Systems
gptkb:Airbus
gptkb:Bell_Helicopter
gptkb:Boeing
gptkb:Thales_Group
|
|
gptkbp:power_output
|
1,000 shp
|
|
gptkbp:power-to-weight_ratio
|
5 shp/kg
|
|
gptkbp:propulsion
|
no
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
15,000 ft
|
|
gptkbp:starting_system
|
starter-generator
|
|
gptkbp:turbine_stage
|
2 stages
|
|
gptkbp:turbine_type
|
free turbine
nickel-based superalloy
|
|
gptkbp:type
|
twin-spool engine
|
|
gptkbp:used_in
|
gptkb:Eurocopter_Tiger
|
|
gptkbp:weight
|
approximately 200 kg
|
|
gptkbp:bfsParent
|
gptkb:Tiger_helicopter
|
|
gptkbp:bfsLayer
|
5
|