Earth satellites. Left at earth orbits, space objects began to pose a threat to functioning spacecraft and, in particular, to stations with crews on board. With the expansion of space exploration the population of space debris began to grow rapidly. It requ...

have resulted in development of nine types of space launch vehicles atop of which more than 1100 spacecraft were orbited as a result of about 500 launches. Yuzhnoye is proud of a lot of successful developments of the space transportation systems, many of which...

assembly and checkout; - ILV prelaunch processing and launch; - complete complex of services for spacecraft (SC). Stationary-based, mobile-based, air-based or sea-based Space Launch Systems may be created depending on the Customer’s requirements and the ILV de...

space applications. The calculation data have a good convergence with test data. Determination of spacecraft aerodynamic characteristics, spacecraft characteristics in solar-wind flux, and solar activity prediction Determination of SC aerodynamic characteristics ...

is primarily used as an aft bay. Transducers Separation switches The switch checks a spacecraft separation event and separation of launch vehicle parts (the switch can be used as an end switch). Relative path sensor The sensor checks a relative p...

Yuzhnoye designs components for spacecraft, taking into account latest engineering achievements and meeting basic space technology requirements: High reliability Compactness Minimum power consumption. The components can be installed with minimum modifications...

Rocket 100-Newton Thruster Cyclone-3 Rocket 30-Newton Thruster Okean-O spacecraft 30-Newton Thruster Cyclone-4 Rocket 30-Newton Thruster Basic Specifications Parameter Cyclone-3 thruster ...

Gas jet propulsion systems (GJPS) damp spacecraft's initial post-separation disturbances and provide attitude control, orbit correction, and spacecraft spin about any axis. Basic Specifications Working medium -  air, nitrogen, argon ...

Gas jet propulsion systems (GJPS) damp spacecraft's initial post-separation disturbances and provide attitude control, orbit correction, and spacecraft spin about any axis. Basic Specifications Working medium -  air, nitrogen, argon ...

phases, the necessity arises of thorough elaboration of these actuators of launch vehicle and spacecraft flight control. The experienced gained in designing and proved technology allow developing analogous units with wide range of characteristics and high ope...