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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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Neighboring Extremal Path Applications for Rocket Trajectory Shaping
30/12/2020
Neighboring Extremal Path Applications for Rocket Trajectory Shaping
A guided rocket system performance is often evaluated by solving an optimal control problem which minimizes a pre-defined objective function, e.g. control effort, while satisfying required boundary conditions. However, rocket...
Finding the Worst-Case Behavior of an Accelerating Rocket due to Side-Wind Disturbances
06/01/2021
Finding the Worst-Case Behavior of an Accelerating Rocket due to Side-Wind Disturbances
Flight control law clearance provides the conditions needed for the system to operate in the stability boundaries. One way to do so is to test all the parameters and variables...
Year End Ceremony & Party
07/01/2021
Year End Ceremony & Party
Graduation ceremony and year-end partyץ Class of 2019-2020
Simulation of the Dynamic Response of Aero-Servo-Elastic Wind-Tunnel Model to Non-Uniform Gust
11/01/2021
Simulation of the Dynamic Response of Aero-Servo-Elastic Wind-Tunnel Model to Non-Uniform Gust
Simulation of dynamic response of Aero-Servo-Elastic Wind-Tunnel model to Non-Uniform gust was conducted. The research is done under the “Gust Load Alleviation techniques assessment on wind tunnel Model of advanced...
Fluid-Structure Interactions with Flapping, Compliant Membrane Wings
18/01/2021
Fluid-Structure Interactions with Flapping, Compliant Membrane Wings
Numerous animals including fish, birds, bats and insects use appendages (fins and wings) with varying levels of flexibility, to provide propulsion and/or weight support as they move through either air...
Construction of Non-Equilibrium Hydrodynamic Models for Atmospheric Entry Plasmas
27/01/2021
Construction of Non-Equilibrium Hydrodynamic Models for Atmospheric Entry Plasmas
The simulation of the aerothermal environment surrounding vehicles moving at hypersonic speed is a complex problem due to its multi-physics and multi-scale nature. Progress in the ability to accurately model...
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...
Events on 30/12/2020
30/12/2020
Neighboring Extremal Path Applications for Rocket Trajectory Shaping
A guided rocket system performance is often evaluated by solving an optimal control problem which minimizes a pre-defined objective function, e.g. control effort, while satisfying required boundary conditions. However, rocket...
Events on 06/01/2021
06/01/2021
Finding the Worst-Case Behavior of an Accelerating Rocket due to Side-Wind Disturbances
Flight control law clearance provides the conditions needed for the system to operate in the stability boundaries. One way to do so is to test all the parameters and variables...
Events on 07/01/2021
07/01/2021
Year End Ceremony & Party
Graduation ceremony and year-end partyץ Class of 2019-2020
Events on 11/01/2021
11/01/2021
Simulation of the Dynamic Response of Aero-Servo-Elastic Wind-Tunnel Model to Non-Uniform Gust
Simulation of dynamic response of Aero-Servo-Elastic Wind-Tunnel model to Non-Uniform gust was conducted. The research is done under the “Gust Load Alleviation techniques assessment on wind tunnel Model of advanced...
Events on 18/01/2021
18/01/2021
Fluid-Structure Interactions with Flapping, Compliant Membrane Wings
Numerous animals including fish, birds, bats and insects use appendages (fins and wings) with varying levels of flexibility, to provide propulsion and/or weight support as they move through either air...
Events on 27/01/2021
27/01/2021
Construction of Non-Equilibrium Hydrodynamic Models for Atmospheric Entry Plasmas
The simulation of the aerothermal environment surrounding vehicles moving at hypersonic speed is a complex problem due to its multi-physics and multi-scale nature. Progress in the ability to accurately model...
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...
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