NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Analysis of Mars Pathfinder Entry Data, Aerothermal Heating, and Heat Shield Material ResponseThe Mars Pathfinder heatshield contained several thermocouples and resistance thermometers. A description of the experiment, the entry data, and analysis of the entry environment and material response is presented. In particular, the analysis addresses uncertainties of the data and the fluid dynamics and material response models. The calculations use the latest trajectory and atmosphere reconstructions for the Pathfinder entry. A modified version of the GIANTS code is used for CFD (computational fluid dynamics) analyses, and FIAT is used for material response. The material response and flowfield are coupled appropriately. Three different material response models are considered. The analysis of Pathfinder entry data for validation of aerothermal heating and material response models is complicated by model uncertainties and unanticipated data-acquisition and processing problems. We will discuss these issues as well as ramifications of the data and analysis for future Mars missions.
Document ID
20020048293
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Milos, Frank
(NASA Ames Research Center Moffett Field, CA United States)
Chen, Y. K.
(NASA Ames Research Center Moffett Field, CA United States)
Tran, H. K.
(NASA Ames Research Center Moffett Field, CA United States)
Rasky, Daniel J.
Date Acquired
August 20, 2013
Publication Date
January 1, 1997
Subject Category
Lunar And Planetary Science And Exploration
Meeting Information
Meeting: 7th AIAA/ASME Joint Thermophysics and Heat Transfer Conference
Location: Albuquerque, NM
Country: United States
Start Date: June 15, 1998
End Date: June 18, 1998
Sponsors: American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers
Funding Number(s)
PROJECT: RTOP 242-80-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available