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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
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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Announcing the appointment of the new Dean, Prof. Gil Iosilevskii
01.01.2026

Announcing the appointment of the new Dean, Prof. Gil Iosilevskii

The Stephen B. Klein Faculty of Aerospace Engineering is pleased to announce a leadership transition.
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Professor Emeritus Dan Givoli has been selected as the 2026 Timoshenko Scholar at Stanford University.
12.11.2025

Professor Emeritus Dan Givoli has been selected as the 2026 Timoshenko Scholar at Stanford University

The Timoshenko Scholar is a prestigious award presented annually in recognition of outstanding contributions to the field of applied mechanics.
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All News
Events
May 06 2026
Research Day 2026
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May 20 2026
Faculty Picnic 2026
The students’ annual event
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All Events
Seminars
May 06 2026
Resilient Decision-Making for Multi-Robot Systems in the Presence of Adversaries
Roee M. Francos is currently a Computer Science Postdoctoral Fellow at the Robotics, Embedded Autonomy, and Communication Theory (REACT) Lab at Harvard University focusing on development of multi-agent resilient decision-making and coordination algorithms. In 2023, he completed his PhD in Computer Science at the Multi-Agent Robotic Systems Laboratory, the Technion-Israel Institute of Technology. He received the B.Sc. in Electrical and Computer Engineering from Ben-Gurion University. His research interests are in multi-agent teamwork, autonomous robotics, intelligent transportation systems, bio-inspired robotics and computer vision, focusing on collaborative algorithms for motion planning of autonomous vehicles, multi-robot learning, and air traffic management and coordination of unmanned vehicles. Roee is a recipient of the 2023 Robotics Science and Systems (RSS) Pioneers Award and the 2025 IEEE Multi-Robot & Multi-Agent Systems (MRS) Young Pioneer Award.
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May 11 2026
Geometric Analysis and Optimization of Doppler-Based Navigation with Low Earth Orbit Satellites
Carlos Caravaca Gallego | This work is towards a Ph.D. degree under the supervision of Prof. Pini Gurfiland and Dr. Hector Rotstein
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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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