|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:country_of_origin
|
gptkb:Russia
|
|
gptkbp:design_purpose
|
gptkb:fighter_aircraft
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
gptkb:RD-33_family
gptkb:RD-33_MK
Brayton cycle
starter motor
|
|
gptkbp:engine_configuration
|
twin-spool
rear-mounted
twin-shaft
|
|
gptkbp:engine_power
|
3,000 hours
|
|
gptkbp:exported_to
|
India, Algeria
|
|
gptkbp:first_flight
|
gptkb:1983
|
|
gptkbp:fuel_economy
|
high
0.85 kg/(k N·h)
|
|
gptkbp:fuel_type
|
kerosene
|
|
gptkbp:history
|
developed from RD-33
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov RD-33 M
|
|
gptkbp:is_tested_for
|
ground testing completed
|
|
gptkbp:length
|
3,800 mm
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:max_speed
|
Mach 2.25
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:notable_users
|
gptkb:Russian_Air_Force
|
|
gptkbp:operational_history
|
in service since 1983
|
|
gptkbp:operational_range
|
2,000 km
|
|
gptkbp:production_status
|
in production
|
|
gptkbp:propulsion
|
no
8,300 lbf
6.9 k N/kg
|
|
gptkbp:related_aircraft
|
Mi G-29, Mi G-35
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:turbine_type
|
axial turbine
|
|
gptkbp:type
|
afterburning turbofan engine
|
|
gptkbp:used_in
|
gptkb:Mikoyan_Mi_G-29
|
|
gptkbp:variant
|
gptkb:RD-33
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Klimov_RD-33
|
|
gptkbp:bfsLayer
|
6
|