Feasibility of rocket propellant production on Mars

Astronomy and Astrophysics – Astronomy

Scientific paper

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Mars, Equipment, Theoretical Studies, Rocket Propellant

Scientific paper

In situ production of rocket propellant to reduce landed mass requirements for Mars return missions has been investigated. The analysis has shown that a system which utilizes atmospheric carbon dioxide and soil moisture to produce liquid methane-oxygen propellant requires a landed mass which is less than half the mass of the ascent vehicle it produces.

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