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THE STEPHEN B. KLEIN FACULTY OF |AEROSPACE ENGINEERING

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About the |Faculty

The Stephen B. Klein Faculty of Aerospace Engineering at the Technion is a world-class academic hub for aeronautics and astronautics, dedicated to creating, expanding, and disseminating ideas and knowledge in aerospace sciences and engineering.
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News
Professor Eli Livne Awarded the 2026 Hanin International Prize
08.02.2026

Professor Eli Livne Awarded the 2026 Hanin International Prize

The late Prof. Meir Hanin International Prize is awarded every two years for significant scientific and/or technological achievements in aerospace sciences.
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Announcing the appointment of the new Dean, Prof. Gil Iosilevskii
01.01.2026

Announcing the appointment of the new Dean, Prof. Gil Iosilevskii

The Stephen B. Klein Faculty of Aerospace Engineering is pleased to announce a leadership transition.
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Professor Emeritus Dan Givoli has been selected as the 2026 Timoshenko Scholar at Stanford University.
12.11.2025

Professor Emeritus Dan Givoli has been selected as the 2026 Timoshenko Scholar at Stanford University

The Timoshenko Scholar is a prestigious award presented annually in recognition of outstanding contributions to the field of applied mechanics.
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All News
Seminars
July 27 2026
The effect of the evaporation process on the combustion properties of nanometric Thermites
Avia Rosenfeld | Nanostructured thermites offer unique opportunities for controlling ignition and energy release through engineered material architectures. This seminar presents the fabrication and characterization of Al/SiO₂ multilayer nanothermites produced by physical vapor deposition and examines their thermal and laser-induced ignition behavior.
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July 29 2026
Mass-transfer dynamics of MOF-801 under forced-flow temperature-swing cycling
Nour Aldeen Nasrallah | Metal-organic frameworks (MOFs) are nanoporous materials with strong potential for sorption-based atmospheric water harvesting, owing to their exceptionally high surface areas (~5,000 m²/g) and easy regeneration at low temperatures (~70 °C). However, their practical implementation is limited by slow heat and mass transport, poor sorbent utilization, and the difficulty of integrating MOF nanopowders into scalable macroscopic thermofluid systems.
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All Seminars
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The effect of the evaporation process on the combustion properties of nanometric Thermites
27/07/2026
The effect of the evaporation process on the combustion properties of nanometric Thermites
Avia Rosenfeld | Nanostructured thermites offer unique opportunities for controlling ignition and energy release through engineered material architectures. This seminar presents the fabrication and characterization of Al/SiO₂ multilayer nanothermites produced by physical vapor deposition and examines their thermal and laser-induced ignition behavior.
Mass-transfer dynamics of MOF-801 under forced-flow temperature-swing cycling
29/07/2026
Mass-transfer dynamics of MOF-801 under forced-flow temperature-swing cycling
Nour Aldeen Nasrallah | Metal-organic frameworks (MOFs) are nanoporous materials with strong potential for sorption-based atmospheric water harvesting, owing to their exceptionally high surface areas (~5,000 m²/g) and easy regeneration at low temperatures (~70 °C). However, their practical implementation is limited by slow heat and mass transport, poor sorbent utilization, and the difficulty of integrating MOF nanopowders into scalable macroscopic thermofluid systems.
Closed-Loop Control of a Dual-Mode Scramjet with Fuel Injection Distribution
17/08/2026
Closed-Loop Control of a Dual-Mode Scramjet with Fuel Injection Distribution
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.
COMBUSTION OF HYPERGOLIC HYBRID ROCKET FUEL IN HYDROGEN PEROXIDE SPRAY ENVIRONMENT
24/08/2026
COMBUSTION OF HYPERGOLIC HYBRID ROCKET FUEL IN HYDROGEN PEROXIDE SPRAY ENVIRONMENT
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.
Data-Driven Modeling of Unsteady Aerodynamics Using Constrained Optimization and Random Input
26/08/2026
Data-Driven Modeling of Unsteady Aerodynamics Using Constrained Optimization and Random Input
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.
Control of a Hypersonic Vehicle with Actuation Bounds and Scramjet Engine Constraints
31/08/2026
Control of a Hypersonic Vehicle with Actuation Bounds and Scramjet Engine Constraints
Omer Wexler | This work is towards an M.Sc. degree under the supervision of Assoc. Prof. Moshe Idan, The Stephen B. Klein Faculty of Aerospace Engineering, Technion
Events on 27/07/2026
27/07/2026
The effect of the evaporation process on the combustion properties of nanometric Thermites
Avia Rosenfeld | Nanostructured thermites offer unique opportunities for controlling ignition and energy release through engineered material architectures. This seminar presents the fabrication and characterization of Al/SiO₂ multilayer nanothermites produced by physical vapor deposition and examines their thermal and laser-induced ignition behavior.
Events on 29/07/2026
29/07/2026
Mass-transfer dynamics of MOF-801 under forced-flow temperature-swing cycling
Nour Aldeen Nasrallah | Metal-organic frameworks (MOFs) are nanoporous materials with strong potential for sorption-based atmospheric water harvesting, owing to their exceptionally high surface areas (~5,000 m²/g) and easy regeneration at low temperatures (~70 °C). However, their practical implementation is limited by slow heat and mass transport, poor sorbent utilization, and the difficulty of integrating MOF nanopowders into scalable macroscopic thermofluid systems.
Events on 17/08/2026
17/08/2026
Closed-Loop Control of a Dual-Mode Scramjet with Fuel Injection Distribution
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.
Events on 24/08/2026
24/08/2026
COMBUSTION OF HYPERGOLIC HYBRID ROCKET FUEL IN HYDROGEN PEROXIDE SPRAY ENVIRONMENT
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.
Events on 26/08/2026
26/08/2026
Data-Driven Modeling of Unsteady Aerodynamics Using Constrained Optimization and Random Input
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.
Events on 31/08/2026
31/08/2026
Control of a Hypersonic Vehicle with Actuation Bounds and Scramjet Engine Constraints
Omer Wexler | This work is towards an M.Sc. degree under the supervision of Assoc. Prof. Moshe Idan, The Stephen B. Klein Faculty of Aerospace Engineering, Technion
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