Technical Papers
Dec 21, 2021

Evaluation of Bosch Process–Sourced Carbon in Low-Carbon Steel and Gray Iron Casting for Martian Surface Manufacturing

Publication: Journal of Aerospace Engineering
Volume 35, Issue 2

Abstract

As research continues for the first crewed missions to and the eventual colonization of Mars, the need for materials for construction of structural and mechanical components remains paramount. The use of in situ resource utilization (ISRU) techniques is critical due to the financial and physical burdens of sending supplies beyond low-Earth orbit. The Bosch process is currently in development as a life-support system at National Aeronautics and Space Administration (NASA) Marshall Space Flight Center (MSFC) to regenerate oxygen (O2) from metabolic carbon dioxide (CO2) with the by-product of elemental carbon (C). In this study, the use of this novel C source for alloying with iron (Fe) to produce ferrous alloys was studied to determine if the Bosch-sourced C could provide similar metallurgical results to a traditional C source. The Bosch C was produced by MSFC through their C-formation reactor (C-Fr) using mill scale (Fe3C) as the reaction catalyst. Two types of ferrous alloys were manufactured using the Bosch-sourced C and a control source C. Mechanical and microstructural properties obtained from each equivalent grade revealed comparable metallurgical results.

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Data Availability Statement

Some or all data, models, or code that support the findings of this study are available from the corresponding author upon reasonable request, including raw material, charge calculations, castings compositions, micrographs, hardness, SEM and XRD, and mechanical testing data.

Acknowledgments

The authors would like to thank the engineers at ECLSS, MSFC for manufacturing and providing the carbon used in this study. The authors also thank Dr. Shane Brauer for his useful guidance pertaining to this work. The authors would like to thank the NASA Technology Transfer Office for the grant (NASA Cooperative Agreement No. NNX17AB32G) that made this research possible. Portions of this study have been presented at the 2019 Materials Science & Technology conference on October 2, 2019, in Portland, Oregon.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 35Issue 2March 2022

History

Received: Jun 3, 2021
Accepted: Nov 10, 2021
Published online: Dec 21, 2021
Published in print: Mar 1, 2022
Discussion open until: May 21, 2022

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Authors

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Blake C. Stewart [email protected]
Graduate Research Assistant, Center for Advanced Vehicular Systems, P.O. Box 5405, Mississippi State, MS 39762; Ph. D. Candidate, Dept. of Mechanical Engineering, Mississippi State Univ., P.O. Box 9552, Mississippi State, MS 39762. Email: [email protected]
Haley R. Doude, Ph.D. [email protected]
Assistant Research Professor, Center for Advanced Vehicular Systems, P.O. Box 5405, Mississippi State, MS 39762. Email: [email protected]
Technology Transfer Office Manager, Marshall Space Flight Center, National Aeronautics and Space Administration, Martin Rd. SW, Huntsville, AL 35808. ORCID: https://orcid.org/0000-0002-6765-3765. Email: [email protected]
Morgan B. Abney, Ph.D. [email protected]
Environmental Control and Life Support System Technical Fellow, Marshall Space Flight Center, National Aeronautics and Space Administration, Martin Rd. SW, Huntsville, AL 35808. Email: [email protected]
Hongjoo Rhee, Ph.D. [email protected]
Associate Director, Center for Advanced Vehicular Systems, P.O. Box 5405, Mississippi State, MS 39762; Associate Professor, Dept. of Mechanical Engineering, Mississippi State Univ., P.O. Box 9552, Mississippi State, MS 39762 (corresponding author). Email: [email protected]

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Cited by

  • Comparison study of ductile iron produced with Martian regolith harvested iron from ionic liquids and Bosch byproduct carbon for in-situ resource utilization versus commercially available 65-45-12 ductile iron, Advances in Space Research, 10.1016/j.asr.2022.10.060, 71, 5, (2175-2185), (2023).

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