|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:AL-31_F
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:controls
|
gptkb:football_match
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
afterburner
|
|
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:engine_type
|
axial
|
|
gptkbp:first_flight
|
gptkb:1982
|
|
gptkbp:fuel_capacity
|
0.85 kg/k N·h
|
|
gptkbp:fuel_type
|
annular
kerosene
|
|
gptkbp:historical_event
|
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:origin
|
gptkb:Russia
|
|
gptkbp:propulsion
|
gptkb:battle
10.25
123 k N
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:used_in
|
gptkb:Sukhoi_Su-27
|
|
gptkbp:variant
|
gptkb:AL-31_F
|
|
gptkbp:weight
|
1,200 kg
|