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Artemis III Extravehicular Activity Science Imaging Use Cases and NeedsAstronaut-acquired photography will provide a critical context for maximizing the scientific return from the extravehicular activities (EVAs) planned for Artemis III. Images will be used to understand the context of crew observations and samples spatially in the exploration area, temporally within the mission timeline, and thematically within the Artemis III science traceability matrix (STM). Both in during the mission in the science evaluation room (SER)and after the mission during curation (preliminary examination and beyond), image data will enable scientific observations and interpretations of the Artemis III landing site. Image data will also be useful for navigation and for monitoring EVA progress and astronaut safety should image data be available in near real time, as well as precise localization during and after the mission. The cameras for Artemis III should be considered an extension of surface science possibilities for the mission. Building on other documents, here we report on our identified use cases and needs concerning the capabilities of these instruments for Artemis III.
Document ID
20250002296
Acquisition Source
Johnson Space Center
Document Type
Abstract
Authors
J M Hurtado, Jr
(The University of Texas at El Paso El Paso, United States)
T L Sweeney
(The University of Texas at El Paso El Paso, United States)
B W Denevi
(Johns Hopkins University Applied Physics Laboratory North Laurel, United States)
C I Fassett
(Johns Hopkins University Applied Physics Laboratory North Laurel, United States)
J Gross
(Johnson Space Center Houston, United States)
Date Acquired
March 4, 2025
Subject Category
Instrumentation and Photography
Meeting Information
Meeting: 56th Lunar and Planetary Science Conference (LPSC)
Location: The Woodlands, TX
Country: US
Start Date: March 10, 2025
End Date: March 14, 2025
Sponsors: Lunar and Planetary Institute
Funding Number(s)
WBS: 964946
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
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