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S.P.Korolev RSC Energia - MARTIAN MISSION





 
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CHRONOLOGICAL EVOLUTION
OF THE MISSION CONCEPT AT RSC ENERGIA

Russian
   
Year of the design Design features
1960
  • Use of electric propulsion for interplanetary transit powered by a 7 MW nuclear reactor;
  • Crew of 6;
  • Delivery to Martian surface of a group of vehicles to make up a self-propelled train
1969
  • Reactor power increased to 15 MW;
  • Crew cut down to 4;
  • Switch to a stationary "headlight"-shaped lander with frontal heat shield
1987
  • Switch to two independent nuclear reactors to increase flight reliability;
  • Changed shape of the lander (lifting body instead of "headlight" with heat shield)
1988
  • Replacement of nuclear power plant with a solar power plant based on a film-type photoelectric converter
1999
  • Modular design for the solar arrays;
  • Changed shape of the lander;
  • Switch from one lander to two (a manned and a logistics lander)

 

  

 

 

 

 

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