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NASA NTRS · 20200002754

Probabilistic Risk Analysis and Margin Process for a Flexible Thermal Protection System

Abstract

Atmospheric entry vehicle thermal protection systems are margined due to the uncertainties that exist in entry aeroheating environments and the thermal response of the materials and structures. Entry vehicle thermal protections systems are traditionally over-margined for the heat loads that are experienced along the entry trajectory by designing to survive stacked worst-case scenarios. Additionally, the conventional heat shield design and margin process offers very little insight into the risk of over-temperature during flight and the corresponding reliability of the heat shield performance. A probabilistic margin process can be used to appropriately margin the thermal protection system based on rigorously calculated risk of failure. This probabilistic margin process allows engineers to make informed aeroshell design, entry-trajectory design, and risk trades while preventing excessive margin from being applied. This study presents the methods of the probabilistic margin process and how the uncertainty analysis is used to determine the reliability of the entry vehicle thermal protection system and associated risks of failure.

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BibTeXRIS

Tobin, Steven A., Brune, Andrew J., Bowes, Angela L. 2019-09-30. Probabilistic Risk Analysis and Margin Process for a Flexible Thermal Protection System. https://ntrs.nasa.gov/citations/20200002754

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