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THE STEPHEN B. KLEIN FACULTY OF |AEROSPACE ENGINEERING

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Max and Desiree Blankfeld Endowed Prize

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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
Events
September 06 2026
Master’s Graduation Ceremony 2026
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September 09 2026
Graduation Ceremony 2026
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September 17 2026
Honoring the Memory of Mark Koifman
The event includes wind tunnel demonstrations, lectures, and lunch. Participation is free of charge, but prior registration is required.
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All Events
Seminars
October 05 2026
Aeroelasticity of Plates with Nonuniform Boundary Conditions Ranging from Pinned to Clamped
Yishai Glam | The aeroelastic stability and dynamic response of thin panels are important considerations in aerospace structures design. Traditional nonlinear Rayleigh-Ritz (RR) analysis struggles when applied to panels with nonuniform boundary conditions (BCs) or local constraints. Generating the necessary global basis functions is difficult, often leading to slow convergence and requiring many modes.
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October 21 2026
Characterization and Modification of the Flow Field Inside Dynamically Evolving Bubbles
Royi Shabtay | The velocity field inside spherical-cap rising bubbles was measured quantitatively by ray-traced, planar laser-induced fluorescence (PLIF) and shadowgraphy and then used to calculate scalar transport properties for bubbles of different Reynolds numbers.
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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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