RT Generic
T1 Simulation of space launcher trajectories
A1 Pérez Pérez, Juan
AB The 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.
YR 2014
FD 2014
LK https://hdl.handle.net/10016/22935
UL https://hdl.handle.net/10016/22935
LA eng
DS e-Archivo
RD 19 may. 2024