DocumentCode :
1231249
Title :
Heat-Shield Ablation and Sublimation Determinations through Radioisotope Techniques
Author :
Brandon, George W. ; Davis, William G.
Author_Institution :
NASA Manned Spacecraft Center Houston, Texas
Issue :
2
fYear :
1965
fDate :
6/1/1965 12:00:00 AM
Firstpage :
278
Lastpage :
283
Abstract :
A technique has been developed for the determination of heat-shield sublimation (char) and surface recession (ablation) during an atmospheric reentry. A radioactive "line" source embedded in the heat-shield material sublimes and ablates at the same rate as the heat shield. Decreases in source activity are monitored by miniaturized nuclear counters. Accuracies exceeding 90 percent are obtainable. The technique provides a continuous indication of char and ablation rates.
Keywords :
Aerospace materials; Automotive engineering; Protection; Radioactive materials; Space exploration; Space heating; Space vehicles; Temperature sensors; Terrestrial atmosphere; Thermal sensors;
fLanguage :
English
Journal_Title :
Aerospace, IEEE Transactions on
Publisher :
ieee
ISSN :
0536-1516
Type :
jour
DOI :
10.1109/TA.1965.4319813
Filename :
4319813
Link To Document :
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