Aerodynamic and aerothermal environment models for a mars entry, descent, and landing systems analysis study

David J. Kinney

doi:10.2514/6.2011-1189

Aerodynamic and aerothermal environment models for a mars entry, descent, and landing systems analysis study

David J. Kinney

Research output: Contribution to conference › Paper › peer-review

5 Scopus citations

Abstract

An NASA in house study of various approaches to landing high mass payloads to the surface of Mars was undertaken by a cross center systems analysis team. Various entry systems capable of landing 40 metric tons of useful payload to the surface of Mars were investigated. This paper will detail the various entry configurations that were investigated and the methods that were used to create the underlying aerodynamic and aerothermal environment models created for the study.

Original language	English
DOIs	https://doi.org/10.2514/6.2011-1189
State	Published - 2011
Externally published	Yes
Event	49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition - Orlando, FL, United States Duration: Jan 4 2011 → Jan 7 2011

Conference

Conference	49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
Country/Territory	United States
City	Orlando, FL
Period	01/4/11 → 01/7/11

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10.2514/6.2011-1189

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abstract = "An NASA in house study of various approaches to landing high mass payloads to the surface of Mars was undertaken by a cross center systems analysis team. Various entry systems capable of landing 40 metric tons of useful payload to the surface of Mars were investigated. This paper will detail the various entry configurations that were investigated and the methods that were used to create the underlying aerodynamic and aerothermal environment models created for the study.",

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AB - An NASA in house study of various approaches to landing high mass payloads to the surface of Mars was undertaken by a cross center systems analysis team. Various entry systems capable of landing 40 metric tons of useful payload to the surface of Mars were investigated. This paper will detail the various entry configurations that were investigated and the methods that were used to create the underlying aerodynamic and aerothermal environment models created for the study.

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M3 - Paper

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Y2 - 4 January 2011 through 7 January 2011

ER -

Aerodynamic and aerothermal environment models for a mars entry, descent, and landing systems analysis study

Abstract

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