הפקולטה |להנדסת אוירונוטיקה וחלל

Shavit Attar | This study demonstrates closed-loop control of the shock train leading-edge location in a dual-mode scramjet combustor using fuel-injection distribution as the control input. Experiments were performed in a direct-connect, cavity-stabilized combustor with distributed ethylene injection.

Saar Levi | Hypergolic propellants are defined by their ability to ignite immediately upon contact, resulting in rapid exothermic reactions occurring without the need for an external ignition source. In hybrid rocket engines, this spontaneous reaction simplifies thruster management, reduces system mass, and enables engine re-ignition.