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Selection, Production, and Properties of Regolith Polymer Composites for Lunar ConstructionNASA’s Artemis Program seeks to establish a long-term presence on the moon to enable scientific discoveries and utilization of lunar resources through public-private partnerships. Over the next decades, a lunar spaceport enabling regular transportation from and to Earth will need to be established to provide the services and facilities that are necessary to achieve this goal. Robotic construction technologies using in-situ materials must be developed to build up enabling infrastructure such as launch/landing pads, blast protection, power/communications towers, improved trafficability pathways and radiation protection shelters. Kennedy Space Center’s Granular Mechanics and Regolith Operations laboratory at Swamp Works has partnered with AI SpaceFactory to develop the architectural and structural design of an unpressurized shelter. The shelter, called Lina, is designed to protect astronauts and surface assets from radiation, meteoroid impact, moon quakes and thermal gradients. Lina’s structural design criteria and the resulting structure design are detailed in separate papers. A Fused Filament Fabrication (FFF) construction process using regolith polymer composites has been developed. This paper presents the material formulations and selection rationale for each of the composite components. Formulations include 70:30, 80:20, and 85:15 wt.% mixture ratios of lunar mare simulant Black Point-1 (BP-1): Polylactic Acid (PLA), 80:20 Lunar Highlands Simulant (LHS-1): PLA and an 80:20 BP-1:PLA formulation with a processing aid/compatibilizer additive. Test samples were printed in simulated lunar dirty thermal vacuum conditions (~-180 °C, ~10-3 torr). The test environment evolved throughout the duration of the print process. A series of tests were performed to characterize the mixture ratios achieved for each formulation, the off-gassing products during vacuum printing, the strength properties, and porosity of printed products. The LHS-1: PLA formulation yielded an advantageous combination of properties and was used in a final test that additively constructed a sub-scaled Lina on regolith simulant in dirty vacuum conditions.
Document ID
20230011080
Acquisition Source
Kennedy Space Center
Document Type
Conference Paper
Authors
Nathan J Gelino
(Kennedy Space Center Merritt Island, Florida, United States)
Tesia Dawn Irwin
(Bionetics (United States) Yorktown, Virginia, United States)
Thomas A Lipscomb
(Engineering Research and Consulting)
Tracy L Gibson
(Engineering Research and Consulting Merritt Island, Florida, United States)
Leonel Herrera
(AI SpaceFactory Merritt Island, Florida, United States)
Laurent Sibille
(Engineering Research and Consulting Merritt Island, Florida, United States)
Evan Allen Bell
(Kennedy Space Center Merritt Island, Florida, United States)
Julian Zoobin Hwang
(OSTEM - Intern)
Date Acquired
July 28, 2023
Subject Category
Engineering (General)
Meeting Information
Meeting: 45th International IEEE Aerospace Conference
Location: Big Sky, MT
Country: US
Start Date: March 2, 2024
End Date: March 9, 2024
Sponsors: Institute of Electrical and Electronics Engineers
Funding Number(s)
WBS: 571232.04.56.76
CONTRACT_GRANT: 80NSSC22DA010
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
Keywords
lunar infrastructure
nasa
radiation shelter
additive construction
regolith polymer composite
meteoroid protection

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