Andrea Mammola
Optimization of hybrid rocket motors for small launchers’ upper-stage.
Rel. Lorenzo Casalino. Politecnico di Torino, Corso di laurea magistrale in Ingegneria Aerospaziale, 2020
|
Preview |
PDF (Tesi_di_laurea)
- Tesi
Licenza: Creative Commons Attribution Non-commercial No Derivatives. Download (2MB) | Preview |
Abstract
The study of rocket engines and motors has become fundamental during last years. In particular the simple idea of “space exploration”, with its political power, has been joined by other more economic aspects. The telecommunications industry is increasingly oriented towards the development of new satellites. That’s why the private industry of launchers is growing more and more, creating a new important market. The necessity of powerful, efficient, environmentally friendly, cheap and safe rockets is the new target in order to send into orbit the heaviest payload at the minimum cost. Just the small launchers industry needs nowadays new solutions, so far little considered, to be optimized.
In particular the frontier of hybrid rockets allows a new approach to propellant combustion that could be revolutionary for future commercial space flights
Relatori
Anno Accademico
Tipo di pubblicazione
Numero di pagine
Corso di laurea
Classe di laurea
URI
![]() |
Modifica (riservato agli operatori) |
