NASA NTRS · 19700025291
Thermo-structural failure limits for the spacecraft component for an Apollo 1B launch environment
Abstract
Computer programs for analyzing aerodynamic heating effects on structural failure of Saturn 1 launch vehicle components
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Faust, C. D., Gillies, A., Posgay, R. G.. 1967-04-25. Thermo-structural failure limits for the spacecraft component for an Apollo 1B launch environment. https://ntrs.nasa.gov/citations/19700025291
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