AL-31 F-M2

URI: https://gptkb.org/entity/AL-31_F-M2

GPTKB entity

Predicate	Object
gptkbp:instance_of	gptkb:jet_engine
gptkbp:application	gptkb:military_aircraft
gptkbp:combustor_type	annular
gptkbp:compressor_type	axial
gptkbp:control_system	gptkb:FADEC digital electronic control
gptkbp:cooling_system	air-cooled
gptkbp:country_of_origin	gptkb:Russia
gptkbp:diameter	1,100 mm
gptkbp:emissions_standard	low
gptkbp:engine	gptkb:AL-31_F gptkb:AL-31_F-M4 gptkb:AL-31_F-M5 gptkb:AL-31_F-M1 gptkb:AL-31_F-M2 gptkb:AL-31_FP Brayton cycle AL-31 F-M3 AL-31 F-M10 AL-31 F-M6 AL-31 F-M7 AL-31 F-M8 AL-31 F-M9
gptkbp:first_flight	gptkb:1982
gptkbp:fuel_economy	0.85 kg/k N·h
gptkbp:fuel_type	kerosene
gptkbp:history	developed from AL-31 F
https://www.w3.org/2000/01/rdf-schema#label	AL-31 F-M2
gptkbp:length	3,800 mm
gptkbp:maintenance	1,000 hours
gptkbp:manufacturer	gptkb:Sukhoi
gptkbp:max_speed	Mach 2.35
gptkbp:noise_level	low
gptkbp:notable_users	gptkb:Russian_Air_Force gptkb:Indian_Air_Force gptkb:Chinese_Air_Force
gptkbp:operational_range	3,000 km
gptkbp:propulsion	yes 10.25 123 k N
gptkbp:reheat_system	afterburner
gptkbp:service_ceiling	15,000 m
gptkbp:turbine_type	axial
gptkbp:type	afterburning turbofan
gptkbp:used_in	gptkb:Sukhoi_Su-27
gptkbp:variant	gptkb:AL-31_F
gptkbp:weight	1,200 kg
gptkbp:bfsParent	gptkb:AL-31_F
gptkbp:bfsLayer	6