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Molecular outgassing measurements for an element of the Shuttle thermal protection systemMolecular outgassing studies were conducted on a thermal-protection material recently developed for the Shuttle Orbiter. Molecular outgassing rates as low as 10 to the minus 11th g/sq cm/sec, condensation coefficients, and molecular desorption rates were measured in four separate experiments using cryogenically and thermoelectrically cooled quartz crystal microbalances. Although the initial outgassing rates are high, they decreased to values in the 10 to the minus 10th g/sq cm/sec range in a reasonable period of time. Outgassing rates do not increase after entry heating although the condensation coefficients at various microbalance collection-surface temperatures become somewhat larger.
Document ID
19760054725
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Visentine, J. T.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Richmond, R. G.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Kelso, R. M.
(NASA Johnson Space Center Houston, Tex., United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1976
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 76-446
Meeting Information
Meeting: Thermophysics Conference
Location: San Diego, CA
Start Date: July 14, 1976
End Date: July 16, 1976
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
76A37691
Distribution Limits
Public
Copyright
Other

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