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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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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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Experimental Aeroelastic Shape Sensing and Control
01/03/2021
Experimental Aeroelastic Shape Sensing and Control
The main goals in aircraft design nowadays are noise and emission reduction, together with performance improvement.  These can be achieved straightforwardly with lightweight, large-span configurations. However, light aircraft are inherently...
Experimentation: Inlet Isolator and Combustor Physics in Scramjets
03/03/2021
Experimentation: Inlet Isolator and Combustor Physics in Scramjets
This talk outlines an effort to understand the impact of inlet isolator physics on the combustion of scramjet engines under actual flight relevant high speed conditions. The objective of the...
Low-Cost Aerial Platform for Guidance, Navigation and Control System Design
10/03/2021
Low-Cost Aerial Platform for Guidance, Navigation and Control System Design
In a general research setting, theoretical models combined with simulation provide the backbone for guidance, navigation, and control systems design. While these are both powerful tools to represent physical systems,...
On the operation of a microjet engine's vaporizer under steady-state conditions
15/03/2021
On the operation of a microjet engine's vaporizer under steady-state conditions
Fuel supply in microjet engines typically makes use of fuel vaporizers. These have a simple design however, their operation involves complicated physics including the disintegration of liquid jet under co-flowing...
Transportation of a Slung Load Using Multiple Multirotors While Maintaining a Constant Altitude Above the Terrain
17/03/2021
Transportation of a Slung Load Using Multiple Multirotors While Maintaining a Constant Altitude Above the Terrain
In recent years, the use of multi-rotors has been drastically increased both in military and civil applications. Specifically, load transportation using a flock of rotary unmanned aerial vehicles (UAVs) has...
Autonomous Classification Under Uncertainty
22/03/2021
Autonomous Classification Under Uncertainty
Classification and object recognition is a fundamental problem in many robotics and aerospace applications, such as autonomous driving, vision-based navigation, and search & rescue. The field has advanced much in...
Plasma Generation and Acceleration Mechanisms in Capillary Capacitive Coupled Radio-Frequency Thruster
24/03/2021
Plasma Generation and Acceleration Mechanisms in Capillary Capacitive Coupled Radio-Frequency Thruster
Capacitively coupled radio-frequency thrusters (CCRFT) are an attractive propulsion option for nanosatellites due to their low operating power, relatively high thrust, and low erosion of the electrodes. Such thrusters can...
Events on 01/03/2021
01/03/2021
Experimental Aeroelastic Shape Sensing and Control
The main goals in aircraft design nowadays are noise and emission reduction, together with performance improvement.  These can be achieved straightforwardly with lightweight, large-span configurations. However, light aircraft are inherently...
Events on 03/03/2021
03/03/2021
Experimentation: Inlet Isolator and Combustor Physics in Scramjets
This talk outlines an effort to understand the impact of inlet isolator physics on the combustion of scramjet engines under actual flight relevant high speed conditions. The objective of the...
Events on 10/03/2021
10/03/2021
Low-Cost Aerial Platform for Guidance, Navigation and Control System Design
In a general research setting, theoretical models combined with simulation provide the backbone for guidance, navigation, and control systems design. While these are both powerful tools to represent physical systems,...
Events on 15/03/2021
15/03/2021
On the operation of a microjet engine's vaporizer under steady-state conditions
Fuel supply in microjet engines typically makes use of fuel vaporizers. These have a simple design however, their operation involves complicated physics including the disintegration of liquid jet under co-flowing...
Events on 17/03/2021
17/03/2021
Transportation of a Slung Load Using Multiple Multirotors While Maintaining a Constant Altitude Above the Terrain
In recent years, the use of multi-rotors has been drastically increased both in military and civil applications. Specifically, load transportation using a flock of rotary unmanned aerial vehicles (UAVs) has...
Events on 22/03/2021
22/03/2021
Autonomous Classification Under Uncertainty
Classification and object recognition is a fundamental problem in many robotics and aerospace applications, such as autonomous driving, vision-based navigation, and search & rescue. The field has advanced much in...
Events on 24/03/2021
24/03/2021
Plasma Generation and Acceleration Mechanisms in Capillary Capacitive Coupled Radio-Frequency Thruster
Capacitively coupled radio-frequency thrusters (CCRFT) are an attractive propulsion option for nanosatellites due to their low operating power, relatively high thrust, and low erosion of the electrodes. Such thrusters can...
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