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
|