|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Sukhoi_Su-34
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
1,500 K
|
|
gptkbp:controls
|
digital control system
|
|
gptkbp:designed_by
|
gptkb:NPO_Saturn
|
|
gptkbp:developer
|
gptkb:1970
gptkb:1980
|
|
gptkbp:diameter
|
1,100 mm
|
|
gptkbp:emissions_standard
|
low emissions
|
|
gptkbp:engine
|
gptkb:AL-31_F-M1
gptkb:AL-31_FP
Brayton cycle
AL-31 F-117 S
AL-31 F-P
|
|
gptkbp:engine_type
|
axial compressor
axial turbine
|
|
gptkbp:first_flight
|
gptkb:1982
|
|
gptkbp:fuel_type
|
kerosene
annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
NPO Saturn AL-31 F
|
|
gptkbp:length
|
3,600 mm
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:NPO_Saturn
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:notable_users
|
gptkb:Russian_Air_Force
gptkb:Indian_Air_Force
gptkb:Kazakh_Air_Force
gptkb:Ukrainian_Air_Force
gptkb:Chinese_Air_Force
|
|
gptkbp:origin
|
gptkb:Russia
|
|
gptkbp:production_years
|
gptkb:1982
present
|
|
gptkbp:propulsion
|
10:1
300 seconds
123 k N
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:supports
|
100 kg/s
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:used_in
|
gptkb:Sukhoi_Su-27
gptkb:Mikoyan_Mi_G-29
|
|
gptkbp:variant
|
gptkb:AL-31_F-M1
AL-31 F-117 S
AL-31 F-P
|
|
gptkbp:weight
|
1,200 kg
|