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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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A Preliminary Design Tool for Optimal Effusion Cooling Holes Diameter and Spacing
03/02/2021
A Preliminary Design Tool for Optimal Effusion Cooling Holes Diameter and Spacing
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...
Measurement and assessment of aerodynamically generated noise inside an airborne structure
15/02/2021
Measurement and assessment of aerodynamically generated noise inside an airborne structure
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...
Automatic landing performance of a civil aircraft in the presence of vertical gusts
17/02/2021
Automatic landing performance of a civil aircraft in the presence of vertical gusts
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...
Nozzle Aerothermodynamic Design for a Plasma Heated Supersonic Wind Tunnel
22/02/2021
Nozzle Aerothermodynamic Design for a Plasma Heated Supersonic Wind Tunnel
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,...
Estimation and Control for Cooperative Slung Load Transportation by a Team of Multirotors
24/02/2021
Estimation and Control for Cooperative Slung Load Transportation by a Team of Multirotors
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...
Experimental Aeroelastic Shape Sensing and Control
01/03/2021
Experimental Aeroelastic Shape Sensing and Control
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...
Experimentation: Inlet Isolator and Combustor Physics in Scramjets
03/03/2021
Experimentation: Inlet Isolator and Combustor Physics in Scramjets
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
03/02/2021
A Preliminary Design Tool for Optimal Effusion Cooling Holes Diameter and Spacing
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
15/02/2021
Measurement and assessment of aerodynamically generated noise inside an airborne structure
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
17/02/2021
Automatic landing performance of a civil aircraft in the presence of vertical gusts
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
22/02/2021
Nozzle Aerothermodynamic Design for a Plasma Heated Supersonic Wind Tunnel
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
24/02/2021
Estimation and Control for Cooperative Slung Load Transportation by a Team of Multirotors
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
01/03/2021
Experimental Aeroelastic Shape Sensing and Control
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
03/03/2021
Experimentation: Inlet Isolator and Combustor Physics in Scramjets
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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