NASA NTRS · 20020086321
NASA's Software Bank (Heath Tecna Aerospace)
Abstract
Heath Tecna Aerospace used a COSMIC program, "Analysis of Filament Reinforced Metal Shell Pressure Vessels," to predict stresses in motorcase walls in a composite hybrid rocket and calculate the ideal geometry for the domes at either end of the filament-wound pressure vessel. The COSMIC program predictions were confirmed in testing.
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1991-01-01. NASA's Software Bank (Heath Tecna Aerospace). https://ntrs.nasa.gov/citations/20020086321
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