YAMAL-200 Communications Satellite
			
  Spacecraft Yamal-100, Yamal-200 were developed by the Corporation 
                      based on the S.P.Korolev RSC Energia-designed Multi-purpose 
                      Satellite Bus under a contract with Gascom within the framework 
                      of the Russian Federal SpaceProgram.
                    
                       
                        |  Yamal-100 SC | 
                         Yamal-200 SC | 
                      
                       
                           | 
                            | 
                      
                    
					
                    Yamal-100 SC of the first modification, that meets the world telecommunications space service market requirements, operated in GEO from September 6, 1999 to August 2011, for the first time having exceeded a ten-year design operating life in GEO, is a demonstrative example of implementing advanced science-intensive space technologies of the XXI century in new developments.
					Yamal-200 is the second, more powerful, modification of the SC design in the Yamal series, and is designed for working 
                      within Yamal satellite communications and broadcasting system,  which provides advanced communications links to organizations 
                      within the Russian gas industry, as well as telecommunications services to users in Russia and abroad, which include voice 
                      and fax communications, videoconferencing, transmission  of digital data and TV programs, connection to the Internet.
					  In the design of these satellites, RSC Energia used its fully developed Multi-purpose Unpressurized Satellite Bus, 
                      allowing, on very short notice, to implement on its basis different special-purpose SC projects (for navigation, Earth 
                      remote sensing, monitoring, etc.) that widely use the modular  principle in their design.
					  
                      
 
					  
                      The Corporation production facilities have the capacity   to manufacture up to 6-8 spacecraft of this type per year. 
                      These facilities meet Russian and international requirements   and standards, have an Assembly-and-Test Center and a High-Cleanliness 
                      Industrial Room that are unparalleled in the Russian rocket     and space industry and also has testing facilities allowing 
                      to run all kinds of tests (strength, vibration, acoustic,      thermal/vacuum integrated electrical tests, etc.) on the 
                      assembled spacecraft in order to verify and guarantee that     their reliability meets customer requirements.
                      Both Yamal-200 SC (SC-1 and SC-2), just like their predecessors,    have undergone a complete scope of tests to develop control 
                      and monitoring interfaces with the Yamal SC Mission Control  Center (MCC), with MCC continuously monitoring SC systems 
                      health from lift-off to the target orbit insertion. The        work and tests incorporated to the maximum extent possible 
                      the lessons learned during development and operation of      Yamal-100 SC, and there were new technical solutions aimed 
                      at assuring a higher reliability and surviveability of the       SC.
					  
                      
 
					  
                      Yamal-200 satellites were launched on November 24, 2003   at 9 hours 22 minutes, Moscow Time. Proton-K launch vehicle 
                      put the orbital module into its reference orbit. The stack of the two spacecraft was delivered from the reference orbit 
                      to the target orbit by an upper stage of the Block DM type   (11C861-01). After Yamal-200 SC stack separates into SC-1 
                      and SC-2, the spacecraft independently transit from the      target orbit into their GEO orbital positions. Both spacecraft 
                      function normally.
                
					  
                     	
				  
                     | Performance    data | 
                         SC-1     | 
                        SC-2      | 
                      
                       
                        | Orbit | 
                          GEO   | 
                            GEO    | 
                      
                       
                        | Mass,     kg | 
                           1360   | 
                            1320     | 
                      
                       
                        Power    supply system output, W: 
                               -during communications 
                          session 
                               -rated | 
                             
                            3580 
                            2800 
                         | 
                           
                            3580 
                            2800 
                         | 
                      
                       
                        | Payload    power, W | 
                            2000   | 
                           2000   | 
                      
                       
                        | The    number of active channels (72 MHz) | 
                              9 (C-band) 
                            6 (Ku-band) 
                         | 
                            18 (C-band)      | 
                      
                       
                        | Launch       vehicle | 
                          Proton with Block DM upper stage 
                            as the 4-th stage (dual satellite launch)    | 
                      
                       
                        | Design    life in orbit, years | 
                               12.25     | 
                            12.25       | 
                      
                       
                        | Orbital    slot | 
                        90°E   | 
                        49°E   |