Turbomeca Turmo IV

URI: https://gptkb.org/entity/Turbomeca_Turmo_IV
GPTKB entity
Statements (31)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application helicopters
gptkbp:combustor_type annular combustion chamber
gptkbp:compression_ratio 12:1
gptkbp:control_system electronic control unit
gptkbp:cooling_system air-cooled
gptkbp:design_date 1960s
gptkbp:diameter 0.4 m
gptkbp:emissions_standard low emissions
gptkbp:engine gptkb:Turbomeca_Astazou
gptkbp:engine_configuration single spool
gptkbp:first_flight gptkb:1960
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 Turmo IV
gptkbp:launch_window starter motor
gptkbp:length 1.2 m
gptkbp:maintenance 500 hours
gptkbp:manufacturer gptkb:Turbomeca
gptkbp:noise_level low noise
gptkbp:operational_range 500 km
gptkbp:power_output 600 k W
gptkbp:propulsion 6.67
800 lbf
gptkbp:successor gptkb:Turbomeca_Arriel
gptkbp:type gptkb:turbofan_engine
gptkbp:used_in gptkb:Aérospatiale_SA_315_Lama
gptkbp:weight 120 kg
gptkbp:bfsParent gptkb:Puma_HC1
gptkbp:bfsLayer 7