Strength of sandwich panels with thin-film facings and foam cores.
- 1 November 1965
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 2 (6), 991-992
- https://doi.org/10.2514/3.28336
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Prediction of design reliability of very large solid-rocket motorsJournal of Spacecraft and Rockets, 1964
- Effectiveness of foam structures for meteoroid protectionJournal of Spacecraft and Rockets, 1964
- The Kolmogorov-Smirnov Test for Goodness of FitJournal of the American Statistical Association, 1951