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

dc.contributor.author	Boussadia, Sohaib
dc.contributor.author	Harchouni, Anis
dc.contributor.author	Bentrad, Hocine (promoteur)
dc.contributor.author	Lamri, Redha ( Promoteur )
dc.date.accessioned	2022-10-16T11:33:29Z
dc.date.available	2022-10-16T11:33:29Z
dc.date.issued	2022
dc.identifier.uri	https://di.univ-blida.dz/jspui/handle/123456789/19824
dc.description	Mémoire de Master option Propulsion Spatiale.-Numéro de Thèse 060/2022	fr_FR
dc.description.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.	fr_FR
dc.language.iso	fr	fr_FR
dc.publisher	Université Blida 01	fr_FR
dc.subject	Propulsion; Combustion	fr_FR
dc.subject	Propergol	fr_FR
dc.subject	Rocket engine	fr_FR
dc.subject	Nozzle	fr_FR
dc.subject	Gas-dynamics	fr_FR
dc.subject	Mechanical engineering,	fr_FR
dc.subject	CAD	fr_FR
dc.title	Conception et réalisation d’un banc d’essai : moteur fusée à propergol solide échelle réduite	fr_FR
dc.type	Thesis	fr_FR