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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
February 11 2026
Integrated Target Allocation and Guidance Strategy using Virtual Targets
Kirill Reznik received his first degree in Mechanical Engineering with a specialization in rocket launch systems from Bauman Moscow State Technical University. He is currently completing his MSc in Aerospace Engineering at the Technion, where his research focuses on cooperative missile guidance under the supervision of Prof. Tal Shima.
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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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All Seminars
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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...
Aft-Sting Mount Effects on Missile Longitudinal Stability and Base Flow Characteristics
09/01/2019
Aft-Sting Mount Effects on Missile Longitudinal Stability and Base Flow Characteristics
Aft-sting mount is the most common method of mounting wind tunnel models when performing aerodynamic (balance) measurements in wind tunnels, especially when testing missile configurations. The influence of this type...
Aeroservoelastic Stability Analysis Using Response-Based Parametric Flutter Margins
14/01/2019
Aeroservoelastic Stability Analysis Using Response-Based Parametric Flutter Margins
At linear flutter onset conditions, an aircraft undergoes self-excited harmonic oscillations in response to any initial trigger, leading to a homogenous frequency-domain flutter equation. Accordingly, common-flutter methods search for the...
Unsteady Supersonic Flow over a Spiked Blunt Body
21/01/2019
Unsteady Supersonic Flow over a Spiked Blunt Body
Blunt nose shapes such as flat-face, hemisphere and ellipse are of supreme interest among the bodies moving at supersonic speeds due to the need for housing payloads, radar or infrared...
2D Particle-In-Cell Simulation of the Narrow Channel Hall Thruster
23/01/2019
2D Particle-In-Cell Simulation of the Narrow Channel Hall Thruster
In the past decade growing numbers of nanosatellites are being used in space, with an-ever increasing mission demands. Nevertheless, due to severe limitations on on-board power, there is currently a...
Combustion of Boron Based Pyrotechnic Compounds
30/01/2019
Combustion of Boron Based Pyrotechnic Compounds
Boron based gelled fuels are promising candidates for certain future ramjet applications, offering potential improvements in performance and/or safety over conventional liquid and solid systems. For this purpose, a fundamental...
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...
Events on 09/01/2019
09/01/2019
Aft-Sting Mount Effects on Missile Longitudinal Stability and Base Flow Characteristics
Aft-sting mount is the most common method of mounting wind tunnel models when performing aerodynamic (balance) measurements in wind tunnels, especially when testing missile configurations. The influence of this type...
Events on 14/01/2019
14/01/2019
Aeroservoelastic Stability Analysis Using Response-Based Parametric Flutter Margins
At linear flutter onset conditions, an aircraft undergoes self-excited harmonic oscillations in response to any initial trigger, leading to a homogenous frequency-domain flutter equation. Accordingly, common-flutter methods search for the...
Events on 21/01/2019
21/01/2019
Unsteady Supersonic Flow over a Spiked Blunt Body
Blunt nose shapes such as flat-face, hemisphere and ellipse are of supreme interest among the bodies moving at supersonic speeds due to the need for housing payloads, radar or infrared...
Events on 23/01/2019
23/01/2019
2D Particle-In-Cell Simulation of the Narrow Channel Hall Thruster
In the past decade growing numbers of nanosatellites are being used in space, with an-ever increasing mission demands. Nevertheless, due to severe limitations on on-board power, there is currently a...
Events on 30/01/2019
30/01/2019
Combustion of Boron Based Pyrotechnic Compounds
Boron based gelled fuels are promising candidates for certain future ramjet applications, offering potential improvements in performance and/or safety over conventional liquid and solid systems. For this purpose, a fundamental...
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