NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Apollo 9 thermal-control-coating degradationAnalytical studies, ground-test data, and flight data before 1967 indicated that degradation of Apollo thermal-control coatings could be expected, possibly to an extent requiring spacecraft design changes to accomplish the worst-case lunar-landing mission. On the Apollo 9 mission, specimens of Apollo thermal-control coatings were retrieved by the astronauts during the extravehicular activity. These specimens were the first to be returned to earth from space unaffected by entry conditions. Subsequent measurements of the thermophysical properties (solar absorptance and hemispherical emittance) of the thermal-control-sample coatings revealed degradation levels well within the design capability of the Apollo spacecraft.
Document ID
19720018214
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Smith, J. A.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1972
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-6863
MSC-S-314
Report Number: NASA-TN-D-6863
Report Number: MSC-S-314
Accession Number
72N25864
Funding Number(s)
PROJECT: RTOP 914-11-00-00-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available