Large scale radio-frequency ion thrusters for manned Mars missions

Computer Science – Performance

Scientific paper

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Manned Mars Missions, Nuclear Electric Propulsion, Rit Engines, Eureca (Esa), Mission Planning, Payload Mass Ratio, Propulsion System Configurations, Propulsion System Performance

Scientific paper

Results of the first part of a mission and system study for manned Mars flights with electric propulsion conducted at the University of Giessen, FRG, are summarized. This part of the study is concerned with a round-trip mission between a high earth orbit and a 1000-km Mars orbit. The propulsion system consists of a cluster of 100-cm-diameter RF ion thruster units supplied by a 40-MW nuclear reactor power plant. The results of the current system and mission analysis demonstrate the advantages of electric propulsion, particularly in terms of high payload ratios.

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