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High purity silica reflective heat shield developmentProgress is reported on the development of a high purity reflective heat shield material. Silicon dioxide was selected as the material because it is highly reflective in the correct wavelength band, has good ablation characteristics, is thermal shock resistant, and is readily fabricated to full size at reasonable cost. Conclusions indicate that: reflectance is affected by purity and morphology; the pure material is readily available; required purity and morphology can be maintained with reasonable care; high reflectances are determined (0.99 from 0.4 to 1.2 microns); major processing steps are defined; and the material appears to be cost effective. It is indicated that the materials are developed to the point of readiness for full scale fabrication and characterization.
Document ID
19750012319
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Blome, J.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1974
Publication Information
Publication: Dynatrend, Inc. Proc. of Outer Planet Probe Technol. Workshop, Sect. 1 through 11
Subject Category
Composite Materials
Accession Number
75N20391
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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