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