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THE STEPHEN B. KLEIN FACULTY OF |AEROSPACE ENGINEERING

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Max and Desiree Blankfeld Endowed Prize

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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
Technion Establishes New International Prize for Transformative Innovation in Aerospace
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.
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Congratulations! Prof. Moshe Idan Promoted to Full Professor
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.
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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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All News
Events
September 06 2026
Master’s Graduation Ceremony 2026
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September 09 2026
Graduation Ceremony 2026
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September 17 2026
Honoring the Memory of Mark Koifman
The event includes wind tunnel demonstrations, lectures, and lunch. Participation is free of charge, but prior registration is required.
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All Events
Seminars
October 05 2026
Aeroelasticity of Plates with Nonuniform Boundary Conditions Ranging from Pinned to Clamped
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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October 21 2026
Characterization and Modification of the Flow Field Inside Dynamically Evolving Bubbles
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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Investigation of a Morphing Wing Capable of Airfoil and Span Adjustment using a Retractable Folding Mechanism – New Engineering Approach
18/10/2017
Investigation of a Morphing Wing Capable of Airfoil and Span Adjustment using a Retractable Folding Mechanism – New Engineering Approach
A morphing or adapting aircraft is a term used to define an airplane that enables mid-flight geometry change, in order to allow a shift in performance and aerodynamic traits which...
Seminar in Memory of Prof. Shmuel and Mrs. Noemi Merhav – Full-State Autopilot & Guidance for Multi-Input Multi-Output Missile Engagements
23/10/2017
Seminar in Memory of Prof. Shmuel and Mrs. Noemi Merhav – Full-State Autopilot & Guidance for Multi-Input Multi-Output Missile Engagements
There are two main approaches to design autopilot and guidance systems: “Single-Loop” and “Two-Loop”. In the “Single-Loop” approach there is no definite autopilot, and the guidance command is applied directly...
Inauguration of ANPL Laboratory
24/10/2017
Inauguration of ANPL Laboratory
Nonlinear Structural and Aerodynamic Modeling for Static Aeroelastic Analysis
25/10/2017
Nonlinear Structural and Aerodynamic Modeling for Static Aeroelastic Analysis
The push towards lighter and more efficient aircraft structures has led to modern aircraft configurations that are more elastic than ever, featuring large elastic deformations in their operating conditions. This trend...
The Timnat Prize Seminar - Experimental Investigation of the Hydrogen Peroxide – Solid Hydrocarbon Hypergolic Ignition
01/11/2017
The Timnat Prize Seminar - Experimental Investigation of the Hydrogen Peroxide – Solid Hydrocarbon Hypergolic Ignition
The research examines the idea of using hypergolic ignition in a hybrid motor. The main advantages of the hybrid motor are the facts that it is simple, controllable and exhibits...
Events on 18/10/2017
18/10/2017
Investigation of a Morphing Wing Capable of Airfoil and Span Adjustment using a Retractable Folding Mechanism – New Engineering Approach
A morphing or adapting aircraft is a term used to define an airplane that enables mid-flight geometry change, in order to allow a shift in performance and aerodynamic traits which...
Events on 23/10/2017
23/10/2017
Seminar in Memory of Prof. Shmuel and Mrs. Noemi Merhav – Full-State Autopilot & Guidance for Multi-Input Multi-Output Missile Engagements
There are two main approaches to design autopilot and guidance systems: “Single-Loop” and “Two-Loop”. In the “Single-Loop” approach there is no definite autopilot, and the guidance command is applied directly...
Events on 24/10/2017
24/10/2017
Inauguration of ANPL Laboratory
Events on 25/10/2017
25/10/2017
Nonlinear Structural and Aerodynamic Modeling for Static Aeroelastic Analysis
The push towards lighter and more efficient aircraft structures has led to modern aircraft configurations that are more elastic than ever, featuring large elastic deformations in their operating conditions. This trend...
Events on 01/11/2017
01/11/2017
The Timnat Prize Seminar - Experimental Investigation of the Hydrogen Peroxide – Solid Hydrocarbon Hypergolic Ignition
The research examines the idea of using hypergolic ignition in a hybrid motor. The main advantages of the hybrid motor are the facts that it is simple, controllable and exhibits...
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