AN OPTIMIZED HYBRID ROCKET MOTOR FOR THE SARA PLATFORM REENTRY SYSTEM DOI 10.5028/jatm.2012.04032312
This paper has described a system design process, based on a multidisciplinary optimization technique, of a conceptual optimized hybrid propellant rocket motor. The proposed engine could be a technological option for the reentry maneuvering system of the Brazilian recoverable satellite (SARA), which...
Salvato in:
| Autori principali: | , , , |
|---|---|
| Natura: | Artigo |
| Lingua: | Inglês |
| Pubblicazione: |
Instituto de Aeronáutica e Espaço (IAE)
2012-10-01
|
| Serie: | Journal of Aerospace Technology and Management |
| Soggetti: | |
| Accesso online: | https://www.jatm.com.br/jatm/article/view/173 |
| Tags: |
Nessun Tag, puoi essere il primo ad aggiungerne!!
|