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The Containment Assurance Risk Framework of the Mars Sample Return ProgramThe Mars Sample Return campaign aims at bringing rock and atmospheric samples from Mars to Earth through a series of robotic missions. These missions would collect the samples being cached and deposited on Martian soil by the Perseverance rover, place them in a container, and launch them into Martian orbit for subsequent capture by an orbiter that would bring them back. Given there exists a non-zero probability that the samples contain biological material, precautions are being taken to design systems that would break the chain of contact between Mars and Earth. These include techniques such as sterilization of Martian particles, redundant containment vessels, and a robust reentry capsule capable of accurate landings without a parachute.
Requirements exist that the probability of containment not assured of Martian-contaminated material into Earth’s biosphere be less than one in a million. To demonstrate compliance with this strict requirement, a statistical framework was developed to assess the likelihood of containment loss during each sample return phase and make a statement about the total combined mission probability of containment not assured. The work presented here describes this framework, which considers failure modes or fault conditions that can initiate failure sequences ultimately leading to containment not assured. Reliability estimates are generated from databases, design heritage, component specifications, or expert opinion in the form of probability density functions or point estimates and provided as inputs to the mathematical models that simulate the different failure sequences. The probabilistic outputs are then combined following the logic of several fault trees to compute the ultimate probability of containment not assured. Given the multidisciplinary nature of the problem and the different types of mathematical models used, the statistical tools needed for analysis are required to be computationally efficient. While standard Monte Carlo approaches are used for fast models, a multi-fidelity approach to rare event probabilities is proposed for expensive models. In this paradigm, inexpensive low-fidelity models are developed for computational acceleration purposes while the expensive high-fidelity model is kept in the loop to retain accuracy in the results. This work presents an example of end-to-end application of this framework highlighting the computational benefits of a multi-fidelity approach.
Document ID
20230006222
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Giuseppe Cataldo
(Goddard Space Flight Center Greenbelt, Maryland, United States)
Amy Braverman
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
Kyle Grello
(Goddard Space Flight Center Greenbelt, Maryland, United States)
Aaron Siddens
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
Kevin Carpenter
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
Date Acquired
April 21, 2023
Subject Category
Lunar and Planetary Science and Exploration
Meeting Information
Meeting: Defense and Aerospace Test and Analysis Workshop (DATAWorks)
Location: Alexandria, VA
Country: US
Start Date: April 25, 2023
End Date: April 27, 2023
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
WBS: 829688.14.02.10.01
CONTRACT_GRANT: 80NM0018D0004
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
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