Guido Saccone

1 ta ish

CIRA Italian Aerospace Research Centre

1. Propulsive and Combustion Modelling of SABRE Engine in Rocket Mode to Support NOx Emissions Estimation in Conceptual Design

   Alessio Ricca, Valeria Borio, Roberta Fusaro +3

   MaqolaRocket and propulsion systems research20240 iqtibos

   ABIABI:AkademIndex/openalex/2024.article.010229