Computer Science – Performance
Scientific paper
Aug 1992
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992wadc.iafcqs...l&link_type=abstract
IAF, International Astronautical Congress, 43rd, Washington, Aug. 28-Sept. 5, 1992. 10 p.
Computer Science
Performance
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.
da Xiaodong
Loeb Hortst W.
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