05 - Propulsion
ANALYSIS AND SIZING OF GREEN PROPULSION SYSTEM FOR A SUBORBITAL AIRCRAFT
M. Bruno¹, R. Cambertoni¹, A. Pellegrino¹, P. Petrachi¹, C. Spampinato¹; ¹Polytechnic of Turin, Italy
The paper deals with achieving an entire propulsion system for a previously designed suborbital aircraft, SALTO I, made up by an airbreathing engine and a rocket engine. We propose a system that can have a focus on green fuels . The main aim is to design a propulsion system which may be a compromise between performances and environmental sustainability.