Sanjurjo Rivo, ManuelPérez Pérez, Juan2016-05-092016-05-0920142014-07-09https://hdl.handle.net/10016/22935The present project will simulate a space launch vehicle trajectory for given launcher and external conditions. It also will give an optimal solution for this trajectory when trajectory parameters are not fixed.application/pdfengAtribución-NoComercial-SinDerivadas 3.0 EspañaAstronáuticaIngeniería aeroespacialSimulaciónLanzadera espacialbachelor thesisAeronáuticaopen access