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High purity silica reflective heat shield developmentA high purity slip cast silica material has been developed for use as a reflective heat shield for entries into the atmospheres of the outer planets. The several stages leading to the development of this material are described and details of raw material selection, preparation of the slip material and casting techniques are discussed. Optical (reflectance and transmittance), physical and chemical properties measurements were performed as a function of the important material and processing variables. Performance analysis of a reflective heat shield fabricated from the high purity silica slip shows that approximately 90 percent of the radiant bow shock energy incident on the heat shield during entry into the atmosphere of Jupiter will be reflected.
Document ID
19750048783
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Blome, J. C.
(McDonnell Douglas Astronautics Co. St. Louis, Mo., United States)
Drennan, D. N.
Schmitt, R. J.
(McDonnell Aircraft Co. St. Louis, Mo., United States)
Date Acquired
August 8, 2013
Publication Date
May 1, 1975
Subject Category
Nonmetallic Materials
Report/Patent Number
AIAA PAPER 75-733
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Thermophysics Conference
Location: Denver, CO
Start Date: May 27, 1975
End Date: May 29, 1975
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
75A32855
Funding Number(s)
CONTRACT_GRANT: NAS2-7897
Distribution Limits
Public
Copyright
Other

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