|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
1,500 K
|
|
gptkbp:certification
|
certified for military use
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:controls
|
digital control system
|
|
gptkbp:cooling_system
|
advanced cooling system
|
|
gptkbp:design
|
engineers from Russia
|
|
gptkbp:designed_by
|
gptkb:Moscow_Machine-Building_Plant
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:elevation
|
up to 15,000 m
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
twin-engine
pylon-mounted
brayton cycle
|
|
gptkbp:engine_type
|
axial compressor
two-stage turbine
|
|
gptkbp:exported_to
|
gptkb:various_countries
|
|
gptkbp:features
|
modular design
|
|
gptkbp:first_flight
|
gptkb:1983
|
|
gptkbp:fuel_capacity
|
good
high fuel consumption
|
|
gptkbp:fuel_type
|
kerosene
|
|
gptkbp:historical_event
|
developed from RD-33
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-33 MK
|
|
gptkbp:is_tested_for
|
extensively tested
|
|
gptkbp:launch_date
|
short startup time
|
|
gptkbp:length
|
3,800 mm
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:market
|
available for export
|
|
gptkbp:modifications
|
gptkb:RD-33_MK-300
gptkb:RD-33_MK-400
gptkb:RD-33_MK-500
|
|
gptkbp:noise_level
|
moderate
|
|
gptkbp:notable_users
|
gptkb:UAE_Air_Force
gptkb:Algerian_Air_Force
gptkb:Russian_Air_Force
gptkb:Indian_Air_Force
gptkb:Kazakh_Air_Force
|
|
gptkbp:number_of_rooms
|
annular combustion chamber
|
|
gptkbp:operational_status
|
gptkb:1983
|
|
gptkbp:origin
|
gptkb:Russia
|
|
gptkbp:performance
|
high performance
|
|
gptkbp:produced_by
|
mass-produced
|
|
gptkbp:propulsion
|
gptkb:battle
6.9
300 seconds
8,300 lbf
90 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:services
|
3,000 hours
|
|
gptkbp:successor
|
gptkb:RD-33
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Mikoyan_Mi_G-29_M
gptkb:Mikoyan_Mi_G-29
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:RD-33
|
|
gptkbp:bfsLayer
|
5
|