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a) b) c) d) Figure 3: Water for electrolysis required at Earth for maneuvers of a) 1 km/s, b) 2 km/s, c) 3 km/s, d) 4 km/s for a 58 t payload, 450 s specific impulse, 80% electrolysis efficiency, and specific solar panel mass of 30 kg/kW. a) b) Figure 4: Water for electrolysis required at Mars for maneuvers of a) 1 km/s, b) 1.5 km/s for a 47 t payload, 450 s specific impulse, 80% electrolysis efficiency and specific solar panel mass of 30 kg/kW. 9 American Institute of Aeronautics and Astronautics Downloaded by NASA LANGLEY RESEARCH CENTRE on January 30, 2018 | http://arc.aiaa.org | DOI: 10.2514/6.2018-1537PDF Image | Water Electrolysis for Propulsion of a Crewed Mars
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