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THE STEPHEN B. KLEIN FACULTY OF |AEROSPACE ENGINEERING

Propelling the Future

Research Labs

Max and Desiree Blankfeld Endowed Prize

Graduate Studies

Industry Relations

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
12.08.2026

Technion Establishes New International Prize for Transformative Innovation in Aerospace

The Max and Desiree Blankfeld Endowed Prize for Transformative Innovation in Aerospace, made possible through a generous gift from Max and Desiree Blankfeld of Houston, Texas.
11.08.2026

Congratulations! Prof. Moshe Idan Promoted to Full Professor

Professor Idan is an internationally recognized researcher whose work has made significant contributions in the areas of estimation theory, flight control systems, and air traffic management.
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.
Events
September 17 2026
The event includes wind tunnel demonstrations, lectures, and lunch. Participation is free of charge, but prior registration is required.
Seminars
August 31 2026
Omer Wexler | Air-breathing hypersonic vehicles (AHVs) have the potential to revolutionize space access and high-speed global transportation. These vehicles can cruise at Mach 5 and above, making them highly attractive for many time-critical applications. Furthermore, by using atmospheric oxygen, they eliminate the need to carry oxidizers. Consequently, AHVs offer increased payload capacities, reusability, and reduced construction and operational costs.
October 05 2026
Yishai Glam | The aeroelastic stability and dynamic response of thin panels are important considerations in aerospace structures design. Traditional nonlinear Rayleigh-Ritz (RR) analysis struggles when applied to panels with nonuniform boundary conditions (BCs) or local constraints. Generating the necessary global basis functions is difficult, often leading to slow convergence and requiring many modes.
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Micro gas turbines generally employ uncooled turbine blades and their thrust is limited by the maximum allowable gas temperature. A miniature cooling scheme embodying effusion cooling may significantly enable higher...
During the design phase of a project, each airborne system is designed and tested in order to demonstrate it can perform under different environmental loads. Acoustic noise is one of...
The commercial aviation industry is motivated to continuously improve landing performance without involving radical changes to aircraft design or operation. In the presence of strong gusts the landing is considered...
High-enthalpy arc-heated supersonic wind tunnels are characterized by test gases that are heated by a high-current electric arc and then expanded and accelerated through a convergent-divergent nozzle. In this work,...
Multirotor UAVs are becoming widespread for both civil and military uses, such as photography, surveillance and payload transportation. A slung load system, in which the payload is connected to several...
The main goals in aircraft design nowadays are noise and emission reduction, together with performance improvement.  These can be achieved straightforwardly with lightweight, large-span configurations. However, light aircraft are inherently...
This talk outlines an effort to understand the impact of inlet isolator physics on the combustion of scramjet engines under actual flight relevant high speed conditions. The objective of the...
Events on 03/02/2021
Micro gas turbines generally employ uncooled turbine blades and their thrust is limited by the maximum allowable gas temperature. A miniature cooling scheme embodying effusion cooling may significantly enable higher...
Events on 15/02/2021
During the design phase of a project, each airborne system is designed and tested in order to demonstrate it can perform under different environmental loads. Acoustic noise is one of...
Events on 17/02/2021
The commercial aviation industry is motivated to continuously improve landing performance without involving radical changes to aircraft design or operation. In the presence of strong gusts the landing is considered...
Events on 22/02/2021
High-enthalpy arc-heated supersonic wind tunnels are characterized by test gases that are heated by a high-current electric arc and then expanded and accelerated through a convergent-divergent nozzle. In this work,...
Events on 24/02/2021
Multirotor UAVs are becoming widespread for both civil and military uses, such as photography, surveillance and payload transportation. A slung load system, in which the payload is connected to several...
Events on 01/03/2021
The main goals in aircraft design nowadays are noise and emission reduction, together with performance improvement.  These can be achieved straightforwardly with lightweight, large-span configurations. However, light aircraft are inherently...
Events on 03/03/2021
This talk outlines an effort to understand the impact of inlet isolator physics on the combustion of scramjet engines under actual flight relevant high speed conditions. The objective of the...
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