Development of downsized bolter robot for lunar structures

dc.contributor.authorMadestam, Jakob
dc.contributor.departmentChalmers tekniska högskola / Institutionen för industri- och materialvetenskapsv
dc.contributor.departmentChalmers University of Technology / Department of Industrial and Materials Scienceen
dc.contributor.examinerAlmefelt, Lars
dc.contributor.supervisorAhlström, Johan
dc.date.accessioned2025-06-09T12:37:40Z
dc.date.issued2025
dc.date.submitted
dc.description.abstractThis master’s thesis project in Product Development at Chalmers University of Technology presents the development of a downsized version of the MMIC-I robot, called mini MMIC-I (mMMIC-I), within NASA’s ARMADAS project. The project was conducted during the spring of 2025 at NASA Ames Research Center in San Francisco, California. ARMADAS focuses on autonomous assembly of large structures in space using modular building blocks (voxels). With the goal of raising the technology readiness level (TRL) of the ARMADAS system and preparing for a potential CubeSat mission, this work investigates the feasibility of scaling down the MMIC-I robot to operate within a 1.5 U voxel size (150 mm x 150 mm x 150 mm). The project followed an agile-inspired product development methodology, combining iterative prototyping, structured evaluation, and reflective learning processes. A two-week sprint structure guided the development timeline, enabling continual feedback and design refinement. The methodology included prototyping with increasing fidelity. Emphasis was placed on balancing fast prototyping cycles with sufficient analytical groundwork to avoid over-engineering within the project’s limited fourmonth duration. During the project, two iterations of mMMIC-I were prototyped and evaluated. While the latest prototype does not perform with the same reliability as MMIC-I, it can be concluded that through further iterations, a version that can perform reliably in 1.5 U voxels is possible. The project also discusses how different aspects of robotic simplification can be applied to the mMMIC-I design and what the required upcoming development steps before flight are.
dc.identifier.coursecodeIMSX30
dc.identifier.urihttp://hdl.handle.net/20.500.12380/309348
dc.language.isoeng
dc.setspec.uppsokTechnology
dc.subjectMMIC-I
dc.subjectARMADAS
dc.subjectRobotics, Lunar
dc.subjectDown-Scaling
dc.subjectRedesign
dc.subjectVoxels
dc.subjectmMMIC-I
dc.subjectNASA
dc.subjectDesign-simplification
dc.titleDevelopment of downsized bolter robot for lunar structures
dc.type.degreeExamensarbete för masterexamensv
dc.type.degreeMaster's Thesisen
dc.type.uppsokH
local.programmeProduct development (MPPDE), MSc

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