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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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BE PART OF THE |AEROSPACE FUTURE

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
August 31 2026
Control of a Hypersonic Vehicle with Actuation Bounds and Scramjet Engine Constraints
Omer Wexler | Air-breathing hypersonic vehicles (AHVs) have the potential to revolutionize space access and high-speed global transportation. These vehicles can cruise at Mach 5 and above, making them highly attractive for many time-critical applications. Furthermore, by using atmospheric oxygen, they eliminate the need to carry oxidizers. Consequently, AHVs offer increased payload capacities, reusability, and reduced construction and operational costs.
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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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Investigation of the Influence of Graphite Additives on the Fuel Regression Rate in Hybrid Propulsion
04/11/2019
Investigation of the Influence of Graphite Additives on the Fuel Regression Rate in Hybrid Propulsion
Hybrid propulsion can be a good alternative to the solid and liquid propellant systems; recently it has been the preferred choice for space tourism missions. In comparison to the solid...
Plasma Propulsion for Space Applications – Technological Trends
06/11/2019
Plasma Propulsion for Space Applications – Technological Trends
In the past two decades, plasma propulsion for space applications has seen an increasing use for all types of satellites, from hefty GEO communications satellites, through tiny cubesats and to...
A Tale of Two Experiments in Unsteady and Turbulent Flows: Boundary Layers and Wind Turbines
11/11/2019
A Tale of Two Experiments in Unsteady and Turbulent Flows: Boundary Layers and Wind Turbines
In this talk I'll present two experimental investigations where unsteady and turbulent flow physics form the common underlying theme. The first study, which is fundamental in nature, was aimed at...
Development of an Ultrasonic Method for Measuring the Ablation Rate and Temperature Distribution within a Silica-Phenolic Thermal Protection Material
13/11/2019
Development of an Ultrasonic Method for Measuring the Ablation Rate and Temperature Distribution within a Silica-Phenolic Thermal Protection Material
Re-entry and hypersonic vehicles, as well as rocket motors, are exposed to extreme heat loads, shear forces and chemically aggressive gasses. To protect the structure of the vehicle, ablative thermal...
Consensus-Based Cooperative Guidance Laws for Simultaneous Target Interception
20/11/2019
Consensus-Based Cooperative Guidance Laws for Simultaneous Target Interception
Guiding a team of pursuers to simultaneously intercept a target (Salvo-attack) is crucial when dealing with modern target defenses. The main objective of the current research is to develop cooperative...
Performance Study of Low-Cost Rocket Controlled by Solenoid
27/11/2019
Performance Study of Low-Cost Rocket Controlled by Solenoid
Currently, among aerospace industries, there is an increasing demand for advancements in rocket precision. Although these systems have provided great technological advancement in this arena, they are accompanied by high...
Events on 04/11/2019
04/11/2019
Investigation of the Influence of Graphite Additives on the Fuel Regression Rate in Hybrid Propulsion
Hybrid propulsion can be a good alternative to the solid and liquid propellant systems; recently it has been the preferred choice for space tourism missions. In comparison to the solid...
Events on 06/11/2019
06/11/2019
Plasma Propulsion for Space Applications – Technological Trends
In the past two decades, plasma propulsion for space applications has seen an increasing use for all types of satellites, from hefty GEO communications satellites, through tiny cubesats and to...
Events on 11/11/2019
11/11/2019
A Tale of Two Experiments in Unsteady and Turbulent Flows: Boundary Layers and Wind Turbines
In this talk I'll present two experimental investigations where unsteady and turbulent flow physics form the common underlying theme. The first study, which is fundamental in nature, was aimed at...
Events on 13/11/2019
13/11/2019
Development of an Ultrasonic Method for Measuring the Ablation Rate and Temperature Distribution within a Silica-Phenolic Thermal Protection Material
Re-entry and hypersonic vehicles, as well as rocket motors, are exposed to extreme heat loads, shear forces and chemically aggressive gasses. To protect the structure of the vehicle, ablative thermal...
Events on 20/11/2019
20/11/2019
Consensus-Based Cooperative Guidance Laws for Simultaneous Target Interception
Guiding a team of pursuers to simultaneously intercept a target (Salvo-attack) is crucial when dealing with modern target defenses. The main objective of the current research is to develop cooperative...
Events on 27/11/2019
27/11/2019
Performance Study of Low-Cost Rocket Controlled by Solenoid
Currently, among aerospace industries, there is an increasing demand for advancements in rocket precision. Although these systems have provided great technological advancement in this arena, they are accompanied by high...
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