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NASA NTRS · 20120004036

Design Study for a Mars Geyser Hopper

Abstract

The Mars Geyser Hopper is a design reference missions (DRMs) for a Discovery-class spacecraft using Advanced Stirling Radioisotope Generator (ASRG) power source. The Geyser Hopper is a mission concept that will investigate the springtime carbon-dioxide geysers found in regions around the south pole of Mars. The Geyser Hopper design uses Phoenix heritage systems and approach, but uses a single ASRG as the power source, rather than twin solar arrays, and is designed to last over a one-year stay on the South Pole. The spacecraft will land at a target landing area near the south pole of Mars, and have the ability to "hop" after a summertime landing to reposition itself close to a geyser site, and wait through the winter until the first sunlight of spring to witness first-hand the geyser phenomenon.

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BibTeXRIS

Landis, Geoffrey A., Oleson, Steven J., McGuire, Melissa. 2012-01-09. Design Study for a Mars Geyser Hopper. https://ntrs.nasa.gov/citations/20120004036

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