Silva, Douglas do NascimentoSantos, Iago Vinicius Macedo2022-04-182022-04-182021-11-19SANTOS, Iago Vinicius Macedo. Avaliação do impacto da densidade no voo de foguetes. 2021. 64f. Dissertação (Mestrado em Engenharia e Ciências Aeroespaciais) - Escola de Ciências e Tecnologia, Universidade Federal do Rio Grande do Norte, Natal, 2021.https://repositorio.ufrn.br/handle/123456789/46983In this present work, the implementation of the ordinary differential equations developed in the literature and which govern the movement of a rocket is presented, with the chosen vehicle being the VS-30 rocket. The code, which is developed in Matlab, is designed so that it is possible to compare the Earth's atmosphere as composed of ideal gas, that is, an atmosphere in which the gases obey the Ideal Gas Law, and in another scenario , like being a type of Van der Waals. The final aim is to verify whether or not there is impact on the flight phenomenon as a whole, applying the Euler method to the solution of the equations already mentioned above.Acesso AbertoApogeuDensidadeGases IdeaisVan der WaalsVS-30masterThesis