Avaliação do impacto da densidade no voo de foguetes
In 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 th...
Spremljeno u:
| Glavni autor: | |
|---|---|
| Daljnji autori: | |
| Format: | Dissertação |
| Jezik: | pt_BR |
| Izdano: |
Universidade Federal do Rio Grande do Norte
|
| Teme: | |
| Online pristup: | https://repositorio.ufrn.br/handle/123456789/46983 |
| Oznake: |
Dodaj oznaku
Bez oznaka, Budi prvi tko označuje ovaj zapis!
|