NASA's Software Bank (Heath Tecna Aerospace)
Originally published in 1991
Body
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.
Full article: http://hdl.handle.net/hdl:2060/20020086321
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.
NASA's Software Bank (Heath Tecna Aerospace)
NASA's Software Bank (Heath Tecna Aerospace)
