RD-33-5

GPTKB entity

Statements (55)
Predicate Object
gptkbp:instance_of gptkb:Team_Rocket
gptkbp:application gptkb:military_aircraft
gptkbp:average_temperature 1500 K
gptkbp:collaborations international collaborations
gptkbp:combustor_type dual-mode combustion
gptkbp:competitors other jet engines
gptkbp:compressor_type axial compressor
gptkbp:control_system gptkb:FADEC
digital control system
gptkbp:cooling_system film cooling
gptkbp:design_features modular design
gptkbp:designed_by gptkb:Moscow_Institute_of_Thermal_Technology
gptkbp:development 5 years
gptkbp:diameter 1.1 m
gptkbp:emissions_standard low
gptkbp:engine gptkb:RD-33
mixed cycle
gptkbp:engine_configuration twin-spool
gptkbp:environmental_impact low
gptkbp:exhaust_system variable area nozzle
gptkbp:exported_to gptkb:various_countries
gptkbp:first_flight gptkb:1983
gptkbp:fuel_economy high
gptkbp:fuel_type kerosene
https://www.w3.org/2000/01/rdf-schema#label RD-33-5
gptkbp:ignition_system gptkb:spark_plug
gptkbp:integration easy integration into aircraft
gptkbp:invention multiple patents filed
gptkbp:is_tested_for completed
gptkbp:length 2.5 m
gptkbp:maintenance 100 hours
gptkbp:manufacturer Klimov
gptkbp:market_share significant market share
gptkbp:noise_level moderate
gptkbp:number_of_rooms 6.5 MPa
gptkbp:operational_cost moderate
gptkbp:operational_range long range
gptkbp:operational_use air superiority fighter
gptkbp:project ongoing research
gptkbp:propulsion 0.5
yes
81 k N
gptkbp:reliability high
gptkbp:safety_features redundant systems
gptkbp:specific_impulse 290 s
gptkbp:status in production
gptkbp:supports ground support equipment
gptkbp:training specialized training
gptkbp:turbine_type axial turbine
gptkbp:type afterburning turbojet engine
gptkbp:upgrades available
gptkbp:used_in gptkb:Mikoyan_Mi_G-29
gptkbp:weight 160 kg
gptkbp:bfsParent gptkb:RD-33_series
gptkbp:bfsLayer 8