Conception et réalisation d’un banc d’essai : moteur fusée à propergol solide échelle réduite

Abstract

Our work consists on making the study and the machining of a solid propellant (fuel) rocket engine at a reduced scale, For that we conceived a test bench adequate to this type of engines, Therefore to determine its performances by measuring the generated thrust in real time during the start up. Followed by a practical part concerning the adaptation of the engine nozzle, which was studied using a continuous flow apparatus on a similar nozzle.