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Ablation of ATJ Graphite at High TemperaturesResults of an extensive experimental program on the ablation of ATJ graphite in air at surface pressures of 0.3 to 4.4 atm and surface temperatures of 2570 to 4030 K are presented. The measured mass-loss rates are correlated with surface temperature, pressure, and effective nose radius. The results are compared with several equilibrium thermochemical ablation theories which differ basically in the chemical species that are considered and in the thermodynamic properties assigned to these species. All the theories predict about the same mass-loss rate in the diffusion-controlled oxidation regime and are in good agreement with the experimental results. At higher temperatures, however, the experimental and theoretical results do not agree. At temperatures above 3700 K, the experimental mass-loss rate becomes independent of pressure and an exponential function of temperature. A comparison of the high-temperature results with the theories indicates that all the theories, except the one based on the thermodynamic properties from the JANAF tables, are invalid because they overpredict the mass-loss rate. On the other hand, the theory based on the JANAF properties underpredicts the measured mass-loss rate by a factor of three at 4000 K. At least a portion of this difference between experiment and theory is attributed to particulate mass loss which is visually observed.
Document ID
19970031174
Acquisition Source
Ames Research Center
Document Type
Reprint (Version printed in journal)
Authors
John H Lundell
(Ames Research Center Mountain View, California, United States)
Robert R Dickey
(Ames Research Center Mountain View, California, United States)
Date Acquired
August 17, 2013
Publication Date
February 1, 1973
Publication Information
Publication: AIAA Journal
Publisher: American Institute of Aeronautics and Astronautics
Volume: 11
Issue: 2
Issue Publication Date: February 1, 1973
ISSN: 0001-1452
e-ISSN: 1533-385X
Subject Category
Nonmetallic Materials
Report/Patent Number
AIAA Paper 71-418
NAS 1.15:112782
NASA-TM-112782
Report Number: AIAA Paper 71-418
Report Number: NAS 1.15:112782
Report Number: NASA-TM-112782
Meeting Information
Meeting: 6th Thermophysics Conference
Location: Tullahoma, TN
Country: US
Start Date: April 26, 1971
End Date: April 28, 1971
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
97N72347
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Thermochemical ablation
Stagnation point
Emissivity
Pyrometer
Convective heat transfer
Contoured nozzles
Heat shield material
Diffusion coefficient
Thermal stresses
Flight testing
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