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Electrodynamic Regolith Conveyor Sub-Orbital Flight ExperimentThe Electrodynamic Regolith Conveyor (ERC) is a technology that is being developed for soil sampling, beneficiation, specialized conveying applications and dust mitigation. The ERC is an extension of the Electrodynamic Dust Shield (EDS). The EDS has been developed for lenses, solar panels, radiators, fabric, and other applications and is scheduled for a technology demonstration mission on the Moon in 2024. The objective of the ERC sub-orbital flight experiment is to perform testing to advance the TRL of the ERC technology by measuring the regolith transport flow rate, power consumption and range of particle trajectories at four different inclinations in a simulated lunar gravity environment. This testing supports discrete element modeling efforts by grounding the simulations with test data.
Document ID
20240013116
Acquisition Source
Kennedy Space Center
Document Type
Presentation
Authors
Aaron Olson
(Kennedy Space Center Merritt Island, Florida, United States)
Date Acquired
October 16, 2024
Subject Category
Lunar and Planetary Science and Exploration
Report/Patent Number
IAC-24-A2.3.2
Meeting Information
Meeting: 75th International Astronautical Congress
Location: Milan
Country: IT
Start Date: October 14, 2024
End Date: October 18, 2024
Sponsors: International Astronautical Federation (IAF)
Funding Number(s)
WBS: 058013.01.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Electrodynamic
Lunar
Conveyor
Regolith
EDS
Sub-Orbital
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