Martian Mission
	 Work Conducted at RSC Energia  to Develop Nuclear Electric Rocket Engines
  
		   The use of nuclear reactors as power plants for electrical    rocket engines (RSC Energia concept till 1988) necessitated 
                      the development of a high-power Nuclear Power Plant (NPP)   based on lithium-niobium technology.
		  The use of nuclear reactors as power plants for electrical    rocket engines (RSC Energia concept till 1988) necessitated 
                      the development of a high-power Nuclear Power Plant (NPP)   based on lithium-niobium technology.
                      The key features of this technology are as follows:
                    
                      -  The electric power source is a fast neutron thermal     emission reactor/converter with thermal emission converters 
                        of heat into electrical power built into its active zone;  
-  Modular design of the active zone and the cooling system   using lithium as a coolant (the structural material is    a niobium alloy);
-  Electrical power distribution system built around specially  designed high-temperature assemblies.
 Thermal emission reactors and nuclear power plants built    on their basis have passed flight tests (on Cosmos 1818 
                      and Cosmos 1867 spacecraft). The properties of a high-power reactor/converter, including nuclear safety issues, were 
                      studied on a physical test stand.
                      More than 200 thermal emission converters have passed tests   in active zones of experimental reactors.
					  
					   
					    RSC Energia built (in 1967) a high-vacuum test facility      for tests on NPP assemblies and systems made of refractory 
                      metals. High-temperature lithium/niobium NPP module prototypes     logged more than 100 000 hours of running time.
					   RSC Energia built (in 1967) a high-vacuum test facility      for tests on NPP assemblies and systems made of refractory 
                      metals. High-temperature lithium/niobium NPP module prototypes     logged more than 100 000 hours of running time.
                      All the major NPP module components and assemblies, as well      as their manufacturing processes have passed developmental 
                      tests using NPP module prototypes. High-temperature electrical   engineering components, including plasma DC voltage converters, 
                      have been built and tested.
                      There has been work done on electric rocket engines, including  development of lithium electric arc jet engines using high-power 
                      electromagnetic plasma acceleration. In one assembly, an   up to 300 kW electric rocket engine was tested.
                      Based on the experience gained in the experiments, RSC Energia has developed designs for space NPPs and electrical power 
                      propulsion units.
                      In spite of the considerable amount of work done in the  NPP development and testing, in 1988, driven by the desire 
                      to make the interplanetary vehicle environmentally safe, a decision was made to switch from nuclear power to solar   power.
              
			        
                       Space nuclear  power plant units and system testing
                           
						  
 
						 
						  
  
                      
						  