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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
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
Seminars
November 16 2026
Radar target classification using RCS characteristics
Eliezer Azoulai | This study investigates the feasibility of classifying anti-tank threats, specifically Rocket-Propelled Grenades (RPGs) and Anti-Tank Guided Missiles (ATGMs), based only on their Radar Cross Section (RCS) characteristics. A comprehensive target RCS database was constructed using electromagnetic simulations, and radar tracking scenarios were simulated to generate dynamic RCS measurements under varying Signal-to-Noise Ratio (SNR) levels and carrier frequencies of 10, 20, and 40 GHz.
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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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