This paper assesses the power requirement for a Manned Mars Rover vehicle. Auxiliary power needs are fulfilled using a hybrid solar photovoltaic/regenerative fuel cell system, while the primary power needs are met using an SP‐100 type reactor. The primary electric power needs, which include 30‐kWe net user power, depend on the reactor thermal power and the efficiency of the power conversion system. Results show that an SP‐100 type reactor coupled to a Free Piston Stirling Engine (FPSE) yields the lowest total vehicle mass and lowest specific mass for the power system. The second lowest mass was for a SP‐100 reactor coupled to a Closed Brayton Cycle (CBC) using He/Xe as the working fluid. The specific mass of the nuclear reactor power systrem, including a man‐rated radiation shield, ranged from 150‐kg/kWe to 190‐kg/kWe and the total mass of the Rover vehicle varied depend upon the cruising speed.

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