|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:AL-31_F
gptkb:NPO_Saturn_AL-31_F
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:controls
|
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:designed_by
|
gptkb:Sukhoi
|
|
gptkbp:diameter
|
1,100 mm
|
|
gptkbp:elevation
|
up to 15,000 m
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
gptkb:Sukhoi
twin-spool
air start
pylon-mounted
|
|
gptkbp:engine_type
|
gptkb:AL-31_F-M1
turbofan
axial
single-stage high-pressure, two-stage low-pressure
|
|
gptkbp:first_flight
|
gptkb:1982
|
|
gptkbp:fuel_capacity
|
1,500 kg
1.1 m
3.8 m
0.85 kg/k N/h
|
|
gptkbp:fuel_type
|
annular
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
AL-31 F-M1
|
|
gptkbp:ignition_system
|
gptkb:park
|
|
gptkbp:length
|
3,800 mm
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_area
|
gptkb:Sukhoi_Su-30
|
|
gptkbp:origin
|
gptkb:Russia
|
|
gptkbp:propulsion
|
gptkb:battle
150 k N
123 k N
|
|
gptkbp:related_to
|
gptkb:AL-31_F
|
|
gptkbp:services
|
3,000 hours
|
|
gptkbp:successor
|
AL-41 F
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:used_in
|
gptkb:Sukhoi_Su-27
|
|
gptkbp:water_source
|
200 kg/h
|
|
gptkbp:weight
|
1,500 kg
|