|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:aircraft_operated
|
gptkb:fighter_aircraft
|
|
gptkbp:certification
|
ISO certified
|
|
gptkbp:combustion_chamber_type
|
annular
|
|
gptkbp:combustion_efficiency
|
high
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
digital
|
|
gptkbp:cooling_system
|
air-cooled
air cooling
|
|
gptkbp:country_of_origin
|
gptkb:Russia
|
|
gptkbp:development
|
gptkb:Klimov_RD-33_M
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:emissions_standard
|
compliant
|
|
gptkbp:engine
|
gptkb:military_aircraft
gptkb:RD-33_MK
available
ongoing
extensive
Brayton cycle
air start
RD series
|
|
gptkbp:engine_configuration
|
gptkb:Klimov_design_bureau
classified
single-spool
83 k N
|
|
gptkbp:engine_power
|
gptkb:5_stars
high performance
3,000 hours
|
|
gptkbp:engine_thrust_vectoring_capability
|
gptkb:none
|
|
gptkbp:engine_type
|
gptkb:RD-33-1
|
|
gptkbp:first_flight
|
gptkb:1985
|
|
gptkbp:fuel_capacity
|
1,200 kg
3.8 m x 1.0 m
|
|
gptkbp:fuel_economy
|
0.85 kg/k N·h
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov RD-33
|
|
gptkbp:is_tested_for
|
completed in 1984
Klimov testing center
|
|
gptkbp:length
|
3,800 mm
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:max_speed
|
Mach 2.25
|
|
gptkbp:noise_level
|
low
yes
|
|
gptkbp:operational_period
|
1985-present
|
|
gptkbp:operational_range
|
1,500 km
|
|
gptkbp:operational_use
|
1990s
|
|
gptkbp:propulsion
|
no
6.92
83 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
18,000 m
|
|
gptkbp:successor
|
gptkb:Klimov_RD-500
|
|
gptkbp:turbine_type
|
axial
|
|
gptkbp:type
|
afterburning turbojet
|
|
gptkbp:used_in
|
gptkb:Mikoyan_Mi_G-29
|
|
gptkbp:water_requirement
|
150 kg/h
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:GE_F414_engine
gptkb:Mikoyan_Mi_G-35
|
|
gptkbp:bfsLayer
|
5
|