About company
History
Development of company
Missiles
Spacecraft
Launch Vehicles
Yuzhnoye Management
Structure
Joint Ventures
Representations
Aerospace Technology
Launch Vehicles
Cyclone
Cyclone-2K
Cyclone-3
Cyclone-4
Zenit
Zenit-2
Zenit-3SL
Zenit-2SLÁ
Zenit-3SLÁ
Dnepr
Mayak
Svitiaz
Spacecraft
Remote Sensing
Micron
MS-2-8
Sich-3-O
Sich-3-R
Communication
Lybid
Lybid-M
Scientific
Interball-Prognoz
Poperedjennia
Rocket Propulsion
Liquid Engines
Sustainers
Liquid rocket engine RD-802
Liquid rocket engine RD-809
Liquid rocket engine RD-858
Liquid rocket engine RD-859
Liquid rocket engine RD-860
Liquid rocket engine RD-861
Liquid rocket engine RD-861K
Liquid rocket engine RD-862
Liquid rocket engine RD-866
Liquid rocket engine RD-868
Vernier Engines
Liquid rocket engine RD-856
Liquid rocket engine RD-855
Liquid rocket engine RD-8
Liquid rocket engine RD-863
Thrusters
Solid Motors
Sustainers
15D206 solid propellant rocket sustainer
15D305 solid propellant rocket sustainer
15D339 solid propellant rocket sustainer
Description
Special-Purpose Motors
Electric Jet Propulsion Systems
D50
AJPS (Ammoniac Jet Propulsion System)
Monopropellant Engines
Gas Jet Propulsion Systems
Aerospace Systems and Components
Rocket components
Sensors
Separation sensor
Relative motion sensor
Flow sensor
Load-Carrying Structures
Frame
Riveted compartement
Pyrotechnical Mechanisms
Pyrofixing Devices
Pyrolocks
Devices of Objects Attachment and Separation from Launch Vehicle
Devices for Holding and Separation of Electric Connectors of Objects Separated
Tanks
Pressure Vessels
Fairings
Cartridge-Pressure Accumulators
Spacecraft Components
Spacecraft Mechanisms
turning device
telescopic gravity booms
separation device
magnetoquers
Antenna Feeder Devices
Power Supply Systems
Pyrotechnical Mechanisms
Propulsion Components
Control Units
Hydraulic throttle
Throttle-distributor of high-temperature gas
Injection valve of high-temperature gas
Inlet valve
Shut-off valve
Shut-off pyrovalve
Pneumopump aggregate
Diaphragm valve
Pressure regulator
Flow governor
Electrohydraulic valve 1
Electrohydraulic valve 2
Electrohydraulic valve 3
Combustion Chambers
Turbopump assemblies
Launch Services
National Economy Products
Power Generation
Gasification and coal firing
Heat Engineering
Electrical Heater
Air-vent Unit Heater
Gas-jets
Electromagnetic valve
Hot-water boilers
Bottom Grids
Environmental Protection Engineering
Industrial Air-cleaners
dust arresters
emulsifiers
exhaust systems
Remotely-operated units
Desalters
Steam generators
Decontamination and disposal
Agricultural Engineering
Combine harvesters
Mining Engineering
Thermoacoustic Plant (Soil pitching)
Urban Transport
Trolley-buses
YuMZ T
E186
Bus
A186
Food Industry Equipment
Medical engineering
Materials and Technologies
Adapters for plain bearings
Bimetallic adapters
Honeycomb structures
Heat insulation
Girders
Metal plastics bottles
Cleanliness control
Barrel Spraying
Rowing oars
Bike wheels
Design and Analytical Support
Air-Gas Dynamic Analysis
Determination of wind aerodynamic loads that affect LV
Determination of LV gasdynamic characteristics at its launch
Determination of spacecraft (SC) aerodynamic characteristics, SC characteristics in solar wind flow, prediction of solar activity.
Calculation of parameters of generator pressurization system of LV tank charged with nitrogen tetroxide (NT) oxidizer.
Calculation of gasdynamic parameters of pneumatic system for aerodynamic payload fairing jettisoning.
Aerodynamic characteristics of LV, LV separating elements and re-entry vehicles.
Aerogasdynamic calculations. Determination of parameters of gases that affect the spacecraft at all ground operation stages as LV part.
Determination of gasdynamic characteristics at staging and spacecraft separation. Gasdynamic designing of separation units.
Calculation of aerodynamic characteristics of wind power units with vertical and horizontal rotation axis.
Modelling and calculation of gas flow parameters in the process of operation of pneumatic systems of various purposes.
Ballistic Design
Ballistic-Navigation Support
Impact Area Determination
Take-off dynamics analysis, separation dynamics analysis…
Reference data on the spacecraft orbiting around the earth
Software Development
Software for automated processing and analysis of test data
Analysis of operational and geometrical parameters of screw pumps
Thermal design
Selection of methods of thermal protection and optimal required thermal protection of launch venicles, spacecraft with the use of engineering approaches based on analysis and generalization of Yuzhnoye SDO's experience
Thermal conditions of propellants during launch vehicle filling and staying on launch pad (heating, evaporation, thermal layering)
Thermal conditions of launch vehicle instruments and electronic systems
Calculation of convective and padiant heating in engine lines
Determination of temperature and humidity conditions around spacecraft on launch vehicle in all phases of operation
Deternimation of launch venicle aerodynamic heating
Thermal conditions of lanuch veniche boby structure
Strength Analysis
Tests
Firing
Firing tests of solid rocket motors
Firing tests of liquid rocket engines
Certification
Liquid Meters and Gas Meters
Strength
Oxygen Control Units
Climatic
Antenna Devices
Innovative Technologies
Anti-Asteroid protection of earth
Sun Key space solar power station
Magnetic-Ion engine
Tourist spacecraft
VITA System
Vibrodiagnostic monitoring
Artillery space launch system
Health and Recreation Centers
News
Digests
Picture Gallery
Contact Address
Yuzhnoye SDO Quality Management System
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