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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
March 25 2026
Focus on the Industry – RAFAEL
RAFAEL will present their Aerospace related activities.
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April 29 2026
Faculty Concert 2026
AE Rocks! Super-talented faculty members and students will play and sing at the 6th Annual Faculty Concert.
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May 20 2026
Faculty Picnic 2026
The students’ annual event
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All Events
Seminars
March 09 2026
Optimal Estimation-Aware Motion: A Control-Centric Optimization Framework
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).
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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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All Seminars
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Electromechanical System for Solid Rocket Motor Thrust Modulation
28/11/2018
Electromechanical System for Solid Rocket Motor Thrust Modulation
The thrust of a solid rocket motor (SRM) mainly depends on the combustion chamber pressure, nozzle geometry and propellant characteristics. The most commonly used method for a prescribed thrust profile...
A Projected Lloyd’s Algorithm for Coverage Control Problems
10/12/2018
A Projected Lloyd’s Algorithm for Coverage Control Problems
This work presents a new approach for solving the coverage problem for large areas given a limited number of sensors. We consider the problem where there is a given area needed...
Transition to Turbulence Over Convex Surfaces and Utilization of Instabilities for Optimal Laminar Separation Delay
17/12/2018
Transition to Turbulence Over Convex Surfaces and Utilization of Instabilities for Optimal Laminar Separation Delay
Understanding flow instability mechanisms in boundary layers is valuable for designing more efficient aerodynamic and hydrodynamic surfaces. This talk consists of two parts; the first discusses instabilities and transition to...
Column Buckling with Non-Ideal Boundary Conditions
19/12/2018
Column Buckling with Non-Ideal Boundary Conditions
Buckling of a slender elastic column under static compressive load is a fundamental and classical problem in structural stability. It has been examined over more than 250 years, starting with...
Study of a Ducted Rocket with a Hybrid Gas Generator
24/12/2018
Study of a Ducted Rocket with a Hybrid Gas Generator
Air-breathing engines as ramjets, scramjets, turbojets, and turbofans have higher specific impulse and energetic performance and, hence, longer range for the same amount of fuel than rockets. Ramjets operate at...
Development of Adaptive Cycle Micro-Turbofan Engine for UAS Applications
26/12/2018
Development of Adaptive Cycle Micro-Turbofan Engine for UAS Applications
The current research is focused around the development of a variable cycle micro-turbofan engine an existing micro-turbojet with less than 1kN thrust. The project involves the conversion of a single...
Nonlinear Aerodynamic Effects on Static Aeroelasticity of Flexible Missiles
31/12/2018
Nonlinear Aerodynamic Effects on Static Aeroelasticity of Flexible Missiles
The general trend in missile development is towards longer, faster, high-maneuverability missiles. This makes missiles increasingly more flexible and therefore more susceptible to aeroelastic effects, such as static and dynamic...
Finding the Shortest 3D paths with Curvature Constraint in Close Range Scenarios
02/01/2019
Finding the Shortest 3D paths with Curvature Constraint in Close Range Scenarios
The problem of finding optimal trajectories is a basic problem in aerospace engineering with many different solution algorithms. One widely investigated branch is the problem of finding shortest paths under...
Events on 28/11/2018
28/11/2018
Electromechanical System for Solid Rocket Motor Thrust Modulation
The thrust of a solid rocket motor (SRM) mainly depends on the combustion chamber pressure, nozzle geometry and propellant characteristics. The most commonly used method for a prescribed thrust profile...
Events on 10/12/2018
10/12/2018
A Projected Lloyd’s Algorithm for Coverage Control Problems
This work presents a new approach for solving the coverage problem for large areas given a limited number of sensors. We consider the problem where there is a given area needed...
Events on 17/12/2018
17/12/2018
Transition to Turbulence Over Convex Surfaces and Utilization of Instabilities for Optimal Laminar Separation Delay
Understanding flow instability mechanisms in boundary layers is valuable for designing more efficient aerodynamic and hydrodynamic surfaces. This talk consists of two parts; the first discusses instabilities and transition to...
Events on 19/12/2018
19/12/2018
Column Buckling with Non-Ideal Boundary Conditions
Buckling of a slender elastic column under static compressive load is a fundamental and classical problem in structural stability. It has been examined over more than 250 years, starting with...
Events on 24/12/2018
24/12/2018
Study of a Ducted Rocket with a Hybrid Gas Generator
Air-breathing engines as ramjets, scramjets, turbojets, and turbofans have higher specific impulse and energetic performance and, hence, longer range for the same amount of fuel than rockets. Ramjets operate at...
Events on 26/12/2018
26/12/2018
Development of Adaptive Cycle Micro-Turbofan Engine for UAS Applications
The current research is focused around the development of a variable cycle micro-turbofan engine an existing micro-turbojet with less than 1kN thrust. The project involves the conversion of a single...
Events on 31/12/2018
31/12/2018
Nonlinear Aerodynamic Effects on Static Aeroelasticity of Flexible Missiles
The general trend in missile development is towards longer, faster, high-maneuverability missiles. This makes missiles increasingly more flexible and therefore more susceptible to aeroelastic effects, such as static and dynamic...
Events on 02/01/2019
02/01/2019
Finding the Shortest 3D paths with Curvature Constraint in Close Range Scenarios
The problem of finding optimal trajectories is a basic problem in aerospace engineering with many different solution algorithms. One widely investigated branch is the problem of finding shortest paths under...
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