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Mars Entry Atmospheric Data System Modeling, Calibration, and Error AnalysisThe Mars Science Laboratory (MSL) Entry, Descent, and Landing Instrumentation (MEDLI)/Mars Entry Atmospheric Data System (MEADS) project installed seven pressure ports through the MSL Phenolic Impregnated Carbon Ablator (PICA) heatshield to measure heatshield surface pressures during entry. These measured surface pressures are used to generate estimates of atmospheric quantities based on modeled surface pressure distributions. In particular, the quantities to be estimated from the MEADS pressure measurements include the dynamic pressure, angle of attack, and angle of sideslip. This report describes the calibration of the pressure transducers utilized to reconstruct the atmospheric data and associated uncertainty models, pressure modeling and uncertainty analysis, and system performance results. The results indicate that the MEADS pressure measurement system hardware meets the project requirements.
Document ID
20140016394
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Karlgaard, Christopher D.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
VanNorman, John
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Siemers, Paul M.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Schoenenberger, Mark
(NASA Langley Research Center Hampton, VA, United States)
Munk, Michelle M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
November 17, 2014
Publication Date
October 1, 2014
Subject Category
Spacecraft Instrumentation And Astrionics
Fluid Mechanics And Thermodynamics
Report/Patent Number
NASA/TM-2014-218535
L-20464
NF1676L-19602
Funding Number(s)
WBS: WBS 757285.01.07.20
Distribution Limits
Public
Copyright
Public Use Permitted.
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