NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The ablation of graphitic materials in the sublimation regime.A large variety of graphitic materials have been tested in an arc heated air stream at a surface pressure of 4.3 atm and a nominal surface temperature of 3925 K. Included were commercial and developmental grades of artificial graphites, both two and three dimensional carbon-carbon composites, composites seeded with refractory compounds, and several special materials such as pyrolytic graphite, mesophase graphite, glassy carbon, and natural graphite. ATJ graphite was used as a control material. Except for the seeded materials which had poor performance, the mass loss rate for all the man-made graphitic materials fell within the range of 17 per cent less to 30 per cent more than the rate for ATJ. Thus it is concluded that wide variations in constituents, processing, fabrication and structure have relatively little effect on the ablation performance of graphitic materials, at least under the conditions of the present tests. Particulate mass loss was observed for all the materials tested and is the dominant mechanism for mass removal at the present test conditions. It is suggested that this mechanism results from physical failure, primarily by compressive thermal stress.
Document ID
19720041569
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lundell, J. H.
Dickey, R. R.
(NASA Ames Research Center Thermal Protection Branch, Moffett Field, Calif., United States)
Date Acquired
August 6, 2013
Publication Date
April 1, 1972
Subject Category
Thermodynamics And Combustion
Report/Patent Number
AIAA PAPER 72-298
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Thermophysics Conference
Location: San Antonio, TX
Start Date: April 10, 1972
End Date: April 12, 1972
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
72A25235
Distribution Limits
Public
Copyright
Other

Available Downloads

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