About the transient filling procedure in a rocket engine reservoir

Abstract

Experimental work plays a mandatory role in today's investigation. It does not only permit to visualize directly the phenomena involved in a process, but also allows to proportionate crucial data so as to validate many computational estimations. Within this frame the thesis here exposed aims to understand and comprehend thanks to experimental techniques and simple but reliable computational calculations the transient lling procedure in a rocket engine reservoir. By doing this some of the most important actuations of this type of engines, like the start-up procedure, will be easily understood.