Abstract

The concept of living off the land by using the indigenous resources of the Moon, Mars, or other potential sites of robotic and human exploration has been termed in situ resource utilization (ISRU) and will be an enabling technology to open up the solar system. Although the most recent National Aeronautics and Space Administration (NASA) human Mars mission study (Design Reference Architecture 5.0) showed that production of propellants and life support consumables was a mission-enabling capability, mission planners were hesitant to select the newly proposed water extraction from Mars soil option because of the perceived high risk associated with this approach. To overcome resistance in putting ISRU capabilities in the critical path of mission success, NASA ISRU developers have adopted the approach of designing and building hardware into end-to-end systems at representative mission scales and testing these systems under mission-relevant conditions at analog field test sites. Previous ISRU field demonstrations have been standalone lunar ISRU modules running on alternating current power with nonoptimal integration. The primary goal of the Mars atmosphere and regolith collector/processor for lander operations (MARCO POLO) project is to design, build, and test an end-to-end first-generation Mars ISRU atmospheric and soil-processing system powered by mission-relevant direct current power while also demonstrating closed-loop power production via the combination of a fuel cell and electrolyzer. A secondary goal is to perform remote and autonomous operations with this integrated system on a 3×3-m(9×9-ft) octagon lander and transfer oxygen and methane produced to a cryocart for use with a thruster to demonstrate an end-to-end Mars resource-to-thrust concept. This paper will outline the overall design, technologies used, and concept of operations for the MARCO POLO project and its upcoming field demonstration.

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References

Heiken, G. H., Vaniman, D. T., French, B. M., and Schmidt, H. H. (1991). Lunar sourcebook: A user’s guide to the Moon, Cambridge University Press, New York.
Keller, B. W., Clark, D. L., and Kirkland, J. A. (2009). “Field test results of the PILOT hydrogen reduction reactor.” AIAA Space 2009 Conf. and Exposition, Pasadena, CA.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 26Issue 1January 2013
Pages: 57 - 66

History

Received: Oct 19, 2011
Accepted: Feb 13, 2012
Published online: Dec 15, 2012
Published in print: Jan 1, 2013

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Michael A. Interbartolo III [email protected]
Project Manager, National Aeronautics and Space Administration (NASA) Johnson Space Center, Mail Code EP, 2101 NASA Parkway, Houston, TX 77058 (corresponding author). E-mail: [email protected]
Gerald B. Sanders [email protected]
Principal Investigator, National Aeronautics and Space Administration (NASA) Johnson Space Center, Mail Code EP, 2101 NASA Parkway, Houston, TX 77058. E-mail: [email protected]
Lara Oryshchyn [email protected]
Soil Processing Module Chief Engineer, National Aeronautics and Space Administration (NASA) Johnson Space Center, Mail Code EP, 2101 NASA Parkway, Houston, TX 77058. E-mail: [email protected]
Software Architect, National Aeronautics and Space Administration (NASA) Johnson Space Center, Mail Code EP, 2101 NASA Parkway, Houston, TX 77058. E-mail: [email protected]
Helen Vaccaro [email protected]
Water Processing Module Chief Engineer, National Aeronautics and Space Administration (NASA) Johnson Space Center, Mail Code EP, 2101 NASA Parkway, Houston, TX 77058. E-mail: [email protected]
Edgardo Santiago-Maldonado [email protected]
Water Cleanup Module Chief Engineer, National Aeronautics and Space Administration (NASA) Kennedy Space Center, Mail Code NE-S-2, Kennedy Space Center, FL 32899. E-mail: [email protected]
Anthony C. Muscatello [email protected]
Atmospheric Processing Module Chief Engineer, National Aeronautics and Space Administration (NASA) Kennedy Space Center, Mail Code NE-S-2, Kennedy Space Center, FL 32899. E-mail: [email protected]

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