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THE STEPHEN B. KLEIN FACULTY OF |AEROSPACE ENGINEERING

Propelling the Future

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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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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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