NASA NTRS · 19790012833
Aerodynamic heating to representative SRB and ET protuberances
Abstract
Heating data and data scaling methods which can be used on representative solid rocket booster and external tank (ET) protuberances are described. Topics covered include (1) ET geometry and heating points; (2) interference heating test data (51A); (3) heat transfer data from tests FH-15 and FH-16; (4) individual protuberance data; and (5) interference heating of paint data from test IH-42. A set of drawings of the ET moldline and protuberances is included.
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Engel, C. D., Lapointe, J. K.. 1979-02-01. Aerodynamic heating to representative SRB and ET protuberances. https://ntrs.nasa.gov/citations/19790012833
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