RD-33-1

GPTKB entity

Statements (54)
Predicate Object
gptkbp:instance_of gptkb:Team_Rocket
gptkbp:application gptkb:military_aircraft
gptkbp:average_temperature up to 1,500 ° C
gptkbp:combustor_type staged combustion
gptkbp:control_system digital electronic control
gptkbp:cooling_system regenerative cooling
gptkbp:design_features modular design
gptkbp:design_purpose maximize performance
gptkbp:designed_by gptkb:Moscow_Institute_of_Thermal_Technology
gptkbp:development gptkb:Soviet_Union
5 years
gptkbp:diameter 1.1 m
gptkbp:emissions_standard low emissions
gptkbp:engine gptkb:RD-33
gptkbp:engine_configuration single shaft
gptkbp:engine_type gptkb:turbofan_engine
gptkbp:exhaust_system variable area nozzle
gptkbp:exported_to gptkb:India
gptkbp:first_flight gptkb:1977
gptkbp:fuel_economy high fuel efficiency
gptkbp:fuel_type kerosene
gptkbp:has_limitations limited to specific aircraft
https://www.w3.org/2000/01/rdf-schema#label RD-33-1
gptkbp:ignition_system gptkb:spark_plug
gptkbp:influenced_by gptkb:RD-500
Western jet engines
gptkbp:involved_technology aerodynamics
gptkbp:is_tested_for extensive testing
gptkbp:key_feature high maneuverability
gptkbp:length 2.5 m
gptkbp:maintenance 1,000 hours
gptkbp:manufacturer Klimov
gptkbp:material lightweight alloys
gptkbp:noise_level low noise
gptkbp:number_of_rooms 6.5 MPa
gptkbp:operational_history used in various conflicts
gptkbp:operational_range high altitude
gptkbp:operational_use combat missions
gptkbp:part_of gptkb:Mi_G-29_family
gptkbp:performance high thrust-to-weight ratio
gptkbp:project next generation engines
gptkbp:propulsion 0.27
81 k N
gptkbp:reliability high reliability
gptkbp:specific_impulse 290 s
gptkbp:status in service
gptkbp:successor gptkb:RD-33_MK
gptkbp:type afterburning turbojet engine
gptkbp:upgrades gptkb:RD-33_series
gptkbp:used_by gptkb:Russian_Air_Force
gptkbp:used_in gptkb:Mikoyan_Mi_G-29
gptkbp:weight 300 kg
gptkbp:bfsParent gptkb:Klimov_RD-33
gptkbp:bfsLayer 6