as promised we’re publishig the final report for the Mission Analysis activities done during the design and development of the Rocksanne I-X sounding rocket. Activity focused mainly on the coding of routines for the prediction of the trajectory achieved with the modeling of the ascent and descent phases. Everything got with the use of Missile Datcom v.97, used for the estimation of the aerodynamics and stability properties.
Everything in the attached report.
Scripts are opensourced on our Github Repository.
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