הפקולטה |להנדסת אוירונוטיקה וחלל

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.

Tamir Gazit | A data-driven methodology is proposed to identify linear unsteady aerodynamic reduced-order models (ROMs) for flexible structures. Constrained gradient-based optimization extracts aerodynamic stiffness, damping, and time-domain convolution kernels directly from input-output data.