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Development of an improved toughness hyperpure silica reflective heat shieldHigh purity three dimensionally woven silica-silica materials were evaluated for use as a tough reflective heat shield for planetary entry probes. A special weave design was selected to minimize light piping effects through the heat shield thickness. Various weave spacings were evaluated for densification efficiency with an 0.7 micron particle size high purity silica. Spectral hemispherical reflectance was measured from 0.2 to 2.5 microns at room temperature. Reflectance increases due to densification and purity of material were measured. Reflectance of 3D hyperpure silica was higher than 3D astroquartz silica for all wavelengths. Mechanical properties were measured in beam flexure and beam shear tests. Results indicated strengths lower than reported for slip cast fused silica. Low strengths were attributed to low densities achieved through vacuum impregnation.
Document ID
19810009571
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rusert, E. L.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Hackett, T. L.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Drennan, D. N.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1979
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-152297
Report Number: NASA-CR-152297
Accession Number
81N18095
Funding Number(s)
CONTRACT_GRANT: NAS2-10003
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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