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                     The Universal Space Platform was developed by S.P. Korolev 
                      RSC Energia within the Yamal project. It has gone flight 
                      qualification as a part of the Yamal-100 communication satellite 
                      launched on September 6, 1999. 
                      Using the Universal Space Platform as the basis, RSC Energia 
                      provides activities in any scope: 
                    
                      -  development and turn-key of communication systems and 
                        Earth remote sensing (ERS) systems as a whole;
 
                       
                      -  development and launch of different-purpose satellites;
 
                       
                      -  platform adaptation as a part of specific space vehicle 
                        of another developer.
 
                     
                    
                       
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                        1999, Baikonur 
                          Yamal-100 spacecraft | 
                        1999, Baikonur 
                          Yamal-100 spacecraft unit | 
                       
                     
                      
                      The Corporation manufacturing plant allows to build up to 
                      6-8 spacecraft of this type per year. The production facilities 
                      meet Russian and international requirements and standards. 
                      For this purpose, a High-Cleanliness Industrial Room was 
                      deployed in the Assembly-and-Test Center of the company, 
                      which is unparalleled in the Russian rocket and space industry. 
                      
                    Key features of the Multi-purpose Satellite 
                      Bus 
                    
                      - No pressurized compartments traditionally used in satellites.
 
                      -  Compartments, solar array panels, on-board antennas 
                        made of sandwiched honeycomb structures based on composite 
                        materials.
 
                      -  Power supply system based on solar arrays and Ni-H 
                        storage batteries
 
                      -  Passive thermal control system using heat pipes.
 
                      -  Motion control system based on optical sensors, high-precision 
                        angular rate meters and momentum wheels
 
                      -  Electrical propulsion unit operating on xenon (liquid- 
                        and gas-based are also possible)
 
                      -  A single on-board control system based on an advanced 
                        computer system which provides a functional unity for 
                        all on-board systems is redundant, and is easily adapted 
                        to the requirements of the specific payload installed 
                        on the bus through the use of specialized software
 
                     
                    The key feature of the design is a pronounced 
                      modularity assuring high manufacturability and ease of the 
                      integration and testing of the Multi-purpose Satellite Bus-based 
                      spacecraft 
                      
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