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Modeling Entry Systems to Explore Our Solar SystemExploration of our Solar System is a foundational element of NASA’s identity. Delivering a scientific payload through an atmosphere to the surface of a planetary body requires safely navigating the extreme temperatures and stresses generated by flying many times the speed of sound. An entry system is the outer shell of a vehicle designed to protect the payload and, as a single point of failure for a mission, reliability is paramount. Unfortunately, it is not possible to fully replicate the flight environment in ground test facilities – so how do we confidently design a vehicle that needs to work the first time, every time? Modeling and simulation are critical tools for filling gaps in ground test capability and providing traceability from ground to flight. Modeling an entry system is a truly interdisciplinary effort, requiring knowledge of fluid dynamics, high-temperature chemistry, radiation, materials science, structural dynamics, guidance and control – and, finally, the mathematical and computing capability to pull it all together. In this talk, Dr. Michael Barnhardt will discuss the latest research in modeling entry systems and how it is being used in NASA’s exploration missions.
Document ID
20220010346
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Michael Barnhardt
(Ames Research Center Mountain View, California, United States)
Aaron Brandis
(Ames Research Center Mountain View, California, United States)
Tom West
(Langley Research Center Hampton, Virginia, United States)
Monica Hughes
(Langley Research Center Hampton, Virginia, United States)
Michael Wright
(Ames Research Center Mountain View, California, United States)
Date Acquired
July 7, 2022
Subject Category
Aeronautics (General)
Engineering (General)
Meeting Information
Meeting: Ames Summer Series
Location: Moffett Field, CA
Country: US
Start Date: July 14, 2022
Sponsors: Ames Research Center
Funding Number(s)
WBS: 335803.04.22.21.10
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
Keywords
Entry systems
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