The design and concept selection of the inherently safe re-entry capsule for the 2 nd Young Engineers' Satellite (YES2) are discussed. A significant investment to evaluate, combine and analyze first the simple ideas is made. The steps define the YES2 concept selection logic include, reduce classes, strip the concept from attributes, merging all the options, and options evaluation and initial design. Material tests were performed and simulation tools were developed for re-entry, heat flux, CFD, FEM, stability, and pressure-shape interaction.
Concept selection and design of the inherently safe re-entry capsule for YES2 / Kruijff, M.; Heide, E. J. V. D.; Dragoni, E.; Castagnetti, D.; Ferretti, S.. - 3:(2003), pp. 1663-1671. (Intervento presentato al convegno 54th International Astronautical Congress of the International Astronautical Federation (IAF), the International Academy of Astronautics and the International Institute of Space Law tenutosi a Bremen, deu nel 2003).
Concept selection and design of the inherently safe re-entry capsule for YES2
Dragoni E.;Castagnetti D.;
2003
Abstract
The design and concept selection of the inherently safe re-entry capsule for the 2 nd Young Engineers' Satellite (YES2) are discussed. A significant investment to evaluate, combine and analyze first the simple ideas is made. The steps define the YES2 concept selection logic include, reduce classes, strip the concept from attributes, merging all the options, and options evaluation and initial design. Material tests were performed and simulation tools were developed for re-entry, heat flux, CFD, FEM, stability, and pressure-shape interaction.
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