TY - GEN
T1 - Simulated Regolith Testing of Origami-Based Covers for Space Robots
AU - Hickey, Brigid
AU - Pierre, Ryan St
N1 - Publisher Copyright:
© 2025 IEEE.
PY - 2025
Y1 - 2025
N2 - A novel benchtop method is presented for evaluating abrasion-induced damage and particulate intrusion in flexible, origami-based covers intended for planetary exploration. Using a rock tumbler with silicon carbide grit as a regolith simulant, this compact, repeatable setup simulates continuous abrasion in a controlled laboratory environment. The protocol enables rapid design iteration by accelerating wear within a 24-hour cycle, making it well suited for earlystage validation of protective structures. Weight measurements and image-based tear analysis were used to assess regolith accumulation and structural failure across cover designs with 3, 4, and 5 pleats. Results found using the proposed approach showed that increased pleat count led to more frequent and distributed tearing, particularly at fold intersections. However, these tears generally reduced particulate accumulation, suggesting a trade-off between flexibility and environmental protection. The approach can be extended to other simulants, including returned regolith, offering a scalable framework for qualifying protective structures in space robotics.
AB - A novel benchtop method is presented for evaluating abrasion-induced damage and particulate intrusion in flexible, origami-based covers intended for planetary exploration. Using a rock tumbler with silicon carbide grit as a regolith simulant, this compact, repeatable setup simulates continuous abrasion in a controlled laboratory environment. The protocol enables rapid design iteration by accelerating wear within a 24-hour cycle, making it well suited for earlystage validation of protective structures. Weight measurements and image-based tear analysis were used to assess regolith accumulation and structural failure across cover designs with 3, 4, and 5 pleats. Results found using the proposed approach showed that increased pleat count led to more frequent and distributed tearing, particularly at fold intersections. However, these tears generally reduced particulate accumulation, suggesting a trade-off between flexibility and environmental protection. The approach can be extended to other simulants, including returned regolith, offering a scalable framework for qualifying protective structures in space robotics.
UR - https://www.scopus.com/pages/publications/105036368486
U2 - 10.1109/iSpaRo66239.2025.11437076
DO - 10.1109/iSpaRo66239.2025.11437076
M3 - Conference contribution
AN - SCOPUS:105036368486
T3 - 2025 International Conference on Space Robotics, iSpaRo 2025
SP - 700
EP - 705
BT - 2025 International Conference on Space Robotics, iSpaRo 2025
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2025 International Conference on Space Robotics, iSpaRo 2025
Y2 - 1 December 2025 through 4 December 2025
ER -