Project Hyreus: Mars sample return mission utilizing in situ propellant production

Computer Science – Performance

Scientific paper

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Carbon Dioxide, Extraterrestrial Resources, Fuel Production, Hydrogen Production, Liquid Rocket Propellants, Mars Sample Return Missions, Mars Surface, Methane, Oxygen Production, Research Projects, Sabatier Reaction, Unmanned Spacecraft, Hydrogen, Mars (Planet), Mars Atmosphere, Mars Probes, Nasa Space Programs, Oxygen, Propulsion System Performance, Voyager Project

Scientific paper

Project Hyreus is an unmanned Mars sample return mission that utilizes propellants manufactured in situ from the Martian atmosphere for the return voyage. A key goal of the mission is to demonstrate the considerable benefits of using indigenous resources and to test the viability of this approach as a precursor to manned Mars missions. The techniques, materials, and equipment used in Project Hyreus represent those that are currently available or that could be developed and readied in time for the proposed launch date in 2003. Project Hyreus includes such features as a Mars-orbiting satellite equipped with ground-penetrating radar, a large rover capable of sample gathering and detailed surface investigations, and a planetary science array to perform on-site research before samples are returned to Earth. Project Hyreus calls for the Mars Landing Vehicle to land in the Mangala Valles region of Mars, where it will remain for approximately 1.5 years. Methane and oxygen propellant for the Earth return voyage will be produced using carbon dioxide from the Martian atmosphere and a small supply of hydrogen brought from Earth. This process is key to returning a large Martian sample to Earth with a single Earth launch.

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