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Deep Space Habitat Primary Structure - A Comparison between Metallic, Inflatable, and Composite MaterialsThis paper presents a comprehensive trade study comparing metallic, inflatable, and composite primary structure materials for a Mars Transit Habitat module. The study evaluates the impact of these materials on the overall mass, outfitting, and mission complexity of the habitat. The results show that the composite module outperforms the other options in terms of minimum mass, being 33% lighter than the metallic configurations and 41% lighter than the inflatable option. The study highlights the potential of composite habitats for future space missions and emphasizes the need for further development and testing to increase the Technology Readiness Level.
Document ID
20240007484
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Matthew T. Ziglar
(Boeing (United States) Chicago, United States)
Michael Elsperman
(Boeing (United States) Chicago, United States)
Date Acquired
June 11, 2024
Subject Category
Composite Materials
Meeting Information
Meeting: ASCEND
Location: Las Vegas, NV
Country: US
Start Date: July 30, 2024
End Date: August 1, 2024
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNH16CO96C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
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