Authors :
Mudra Patil
Volume/Issue :
Volume 10 - 2025, Issue 7 - July
Google Scholar :
https://tinyurl.com/kcpypm4a
Scribd :
https://tinyurl.com/3ym858pd
DOI :
https://doi.org/10.38124/ijisrt/25jul1969
Note : A published paper may take 4-5 working days from the publication date to appear in PlumX Metrics, Semantic Scholar, and ResearchGate.
Abstract :
In-Space Manufacturing and Assembly (ISAM) is a growing field that requires highly reliable systems which are
capable of operating in space. This paper explores the application of Poka-Yoke (mistake-proofing) techniques in the design
of deployment mechanisms for ISAM. This study shows how Poka-Yoke can significantly enhance reliability of deployment
systems in space through systematic integration of asymmetric features, interlocking geometries, passive alignment, and
mechanical sequencing. The proposed design framework is built within the scope of Design for In-Space Manufacturability
(DFISM) principles.
Keywords :
In-Space Manufacturing & Assembly, Design for in-Space Manufacturability, Poka-Yoke.
References :
- Y. Kim, et al., "Design Considerations for Robotic Assembly in Orbit," Acta Astronautica, vol. 190, pp. 50-60, 2021.
- J. Lamoureux and M. Dubey, "Application of Poka-Yoke in Autonomous Assembly," International Journal of Advanced Manufacturing Technology, vol. 105, pp. 2109-2123, 2019.
- S. Thangavelu, "Design for Space Operations: DFISM Framework," Space Manufacturing Conference Proceedings, 2022.
- Keller, "Compliant Mechanisms in Aerospace," Aerospace Mechanisms Symposium, NASA, 2020.
- N. Grompone, et al., "Deployable Structures for Space Applications," Journal of Aerospace Engineering, vol. 234, no. 7, pp. 1123-1140, 2020.
In-Space Manufacturing and Assembly (ISAM) is a growing field that requires highly reliable systems which are
capable of operating in space. This paper explores the application of Poka-Yoke (mistake-proofing) techniques in the design
of deployment mechanisms for ISAM. This study shows how Poka-Yoke can significantly enhance reliability of deployment
systems in space through systematic integration of asymmetric features, interlocking geometries, passive alignment, and
mechanical sequencing. The proposed design framework is built within the scope of Design for In-Space Manufacturability
(DFISM) principles.
Keywords :
In-Space Manufacturing & Assembly, Design for in-Space Manufacturability, Poka-Yoke.