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The Planetary Protection Strategy of Mars Sample Return’s Earth Return Orbiter MissionThe Mars Sample Return campaign aims to use three flight missions and one ground element to safely bring rock cores, regolith and atmospheric samples from the surface of Mars to Earth to answer key questions about the geologic and climate history of Mars, including the potential for ancient life. Since its landing in Jezero Crater in 2021, the first mission, NASA’s Mars 2020, has collected a number of samples on the crater floor and on the delta using the Perseverance rover. Subsequent missions would recover the sealed sample tubes, launch them into Mars orbit, and transport them back to Earth. The ground element would be a high-containment facility that would isolate and protect the samples during initial sample characterization, which would include sample safety assessments and time-sensitive scientific investigations. These elements are currently in the planning and design stages of development, and represent an international effort of NASA, the European Space Agency (ESA), and many industry partners. The work presented here provides an overview of the planetary protection strategy of the third flight mission, the ESA-led Earth Return Orbiter, which hosts the NASA-provided Capture, Containment, and Return System. The orbiter would detect and capture the container with up to 30 sealed tubes previously put in Martian orbit, contain them in redundant containers to ensure that no potentially hazardous Mars particles are released, and return them to Earth through an entry vehicle. Both NASA and ESA policies comply with the United Nations’ Outer Space Treaty by planning to protect Earth’s biosphere from any potential adverse effects from material returned from solar system bodies beyond the Earth-Moon system. In the conduct of Mars Sample Return, the two agencies have mutually agreed to apply approaches consistent with their own planetary protection standards to the campaign elements they each provide.
Document ID
20240003360
Acquisition Source
Goddard Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Giuseppe Cataldo
(Goddard Space Flight Center Greenbelt, United States)
Lorenz Affentranger
(European Space Agency Paris, France)
Brian G Clement
(Jet Propulsion Laboratory La Cañada Flintridge, United States)
Daniel P. Glavin
(Goddard Space Flight Center Greenbelt, United States)
David W Hughes
(Goddard Space Flight Center Greenbelt, United States)
John Hall
(European Space Agency Paris, France)
Bruno Sarli
(Heliospace Corporation Berkeley, CA)
Christine E Szalai
(Jet Propulsion Laboratory La Cañada Flintridge, United States)
Date Acquired
March 19, 2024
Publication Date
May 15, 2024
Publication Information
Publication: Journal of Space Safety Engineering
Publisher: Elsevier
Volume: 11
Issue: 2
Issue Publication Date: June 8, 2024
ISSN: 2468-8975
e-ISSN: 2468-8967
Subject Category
Lunar and Planetary Science and Exploration
Funding Number(s)
WBS: 829688.14.02.10.01
CONTRACT_GRANT: 80NM0018D0004
CONTRACT_GRANT: 80HQTR21D0003
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
Keywords
Mars Sample Return
Earth Return Orbiter
Planetary Protection
Break the Chain
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