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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.

BE PART OF THE |AEROSPACE FUTURE

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
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.
October 21 2026
Royi Shabtay | The velocity field inside spherical-cap rising bubbles was measured quantitatively by ray-traced, planar laser-induced fluorescence (PLIF) and shadowgraphy and then used to calculate scalar transport properties for bubbles of different Reynolds numbers.
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Dr. Liraz Mudrik is currently a Postdoctoral Fellow in the Department of Mechanical and Aerospace Engineering at the Naval Postgraduate School. He received his Ph.D. in Aerospace Engineering (direct track) from the Technion–Israel Institute of Technology in 2023, where he also earned his B.Sc. (cum laude).
A PostDoctoral Seminar by Eyal Baruch: As space missions such as solar sails, reflector antennas and solar arrays increase in size, their dynamics become ever more important, since large deflections can lead to efficiency loss, damage, or stability loss. The first step in addressing these problems is the accurate identification of system dynamics, most notably vibration mode shapes, natural frequencies, and damping ratios. However, these systems often cannot be tested at full scale prior to deployment, and numerical simulations may overlook key components, such as the correct damping mechanisms. This problem is further intensified by the complexity of carbon fiber thin shells, which serve as the fundamental building blocks of ultralight deployable structures. For such systems, classical similitude methods such as dimensional analysis (DA) are inapplicable, since parameters such as shell thickness and the stiffness matrix cannot be experimentally scaled.
Events on 11/03/2026
Charles Touitou has been an MSc student in the Faculty of Aerospace Engineering since 2024 and currently works as an aerodynamics engineer at Elbit Systems.
Events on 18/03/2026
Dr. Liraz Mudrik is currently a Postdoctoral Fellow in the Department of Mechanical and Aerospace Engineering at the Naval Postgraduate School. He received his Ph.D. in Aerospace Engineering (direct track) from the Technion–Israel Institute of Technology in 2023, where he also earned his B.Sc. (cum laude).
Events on 30/03/2026
A PostDoctoral Seminar by Eyal Baruch: As space missions such as solar sails, reflector antennas and solar arrays increase in size, their dynamics become ever more important, since large deflections can lead to efficiency loss, damage, or stability loss. The first step in addressing these problems is the accurate identification of system dynamics, most notably vibration mode shapes, natural frequencies, and damping ratios. However, these systems often cannot be tested at full scale prior to deployment, and numerical simulations may overlook key components, such as the correct damping mechanisms. This problem is further intensified by the complexity of carbon fiber thin shells, which serve as the fundamental building blocks of ultralight deployable structures. For such systems, classical similitude methods such as dimensional analysis (DA) are inapplicable, since parameters such as shell thickness and the stiffness matrix cannot be experimentally scaled.
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