Material Response Modeling of MMOD Cavities

Olivia M. Schroeder, Prakash Shrestha, Grant Palmer, Eric Stern, Graham V. Candler

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

There is an increasing need to predictively model failure modes for thermal protection systems (TPS) driven by high mission reliability requirements as well as increasingly complex or extreme planetary entries. One potential failure mode could arise from TPS damage resultant from a micro-meteoroid or orbital debris strike. This work focuses on modeling fluid dynamics and material response of a FiberForm test article with cavities in a high enthalpy flow environment. Specifically, an arc-jet experiment in the Aerodynamic Heating Facility (AHF) is taken as a baseline simulation upon which a parametric study is built. The study investigates the thermal response of the material under various cavity geometric configurations with two focuses: cavity depth and cavity shape. The influence of these parameters on the bondline temperature is assessed.

Original languageEnglish (US)
Title of host publicationAIAA SciTech Forum 2022
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624106316
DOIs
StatePublished - 2022
EventAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 - San Diego, United States
Duration: Jan 3 2022Jan 7 2022

Publication series

NameAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022

Conference

ConferenceAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Country/TerritoryUnited States
CitySan Diego
Period1/3/221/7/22

Bibliographical note

Funding Information:
The primary author is funded by a NASA Space Technology Research Fellowship (NSTRF)) under Grant Number 80NSSC18K1150. Support from ONR MURI Grant number N00014-20-1-2682 is also acknowledged. Additional support provided by NASA’s Mars Sample Return Earth Entry Vehicle (MSR-EEV) project, and the Space Technology Mission Directorate (STMD) Entry Systems Modeling (ESM) project.

Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc.. All rights reserved.

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