Contact Us

THE STEPHEN B. KLEIN FACULTY OF |AEROSPACE ENGINEERING

Propelling the Future

Research Labs

Max and Desiree Blankfeld Endowed Prize

Graduate Studies

Industry Relations

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.
FACULTY POSITIONS
GRADUATE RESEARCH OPPORTUNITIES
ADMISSION

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.
Read More
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.
Read More
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.
Read More
All News
Events
September 06 2026
Master’s Graduation Ceremony 2026
Read more
September 09 2026
Graduation Ceremony 2026
Read more
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.
Read more
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.
Read more
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.
Read more
All Seminars
Today
Sun
Mon
Tue
Wed
Thu
Fri
Sat
S
M
T
W
T
F
S
26
27
28
29
30
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
1
2
3
4
5
6
The Third Annual Professor Singer Memorial Lecture
03/07/2016
The Third Annual Professor Singer Memorial Lecture
Satellite Collision Awareness and Avoidance
06/07/2016
Satellite Collision Awareness and Avoidance
Spacecraft formation and cluster flight control have seen growing interest in the last decade. However, the problem of finding the optimal debris collision avoidance maneuver for a member of a...
On the conversion of Gas Turbine Combustors – Low Swirl Injection
11/07/2016
On the conversion of Gas Turbine Combustors – Low Swirl Injection
The research work will discuss investigations into the characteristics of Low Swirl Injector (LSI) technique as a viable modification to be used in the conversion of liquid fuelled aero-engines to...
Thermodynamic Simulation of a Continuous Closed Loop Heated Micro-Turbine Test Facility
13/07/2016
Thermodynamic Simulation of a Continuous Closed Loop Heated Micro-Turbine Test Facility
This incremental development project is focused around a versatile continuously-running high-speed micro gas turbine research facility, which is capable of matching full engine similarity conditions including pressure loading (synonymous with...
A Low-Cost Laser-Range-Measurement Based Terrain-Following Concept and Error Analysis
20/07/2016
A Low-Cost Laser-Range-Measurement Based Terrain-Following Concept and Error Analysis
This seminar addresses the design and error assessment and analysis of a low cost terrain following system for UAVs. Such a system enables an aircraft to maintain a pre-defined vertical...
Negotiation Between Dynamical Systems with Connectivity Constraints
27/07/2016
Negotiation Between Dynamical Systems with Connectivity Constraints
Multi-agent systems (MAS) have been an important area of study over the past few years. This research will propose a real time sub-optimal solution for an agreement problem in multi-agent...
Micro-Turbojet to Turbofan Conversion via Continuously Variable Transmission: Thermodynamic Performance Study
03/08/2016
Micro-Turbojet to Turbofan Conversion via Continuously Variable Transmission: Thermodynamic Performance Study
In this study, the viability, performance, and characteristics of a turbojet-to-turbofan conversion through the use of a continuously variable transmission (CVT) are investigated. By an in-house thermodynamic simulation code, the...
Events on 03/07/2016
03/07/2016
The Third Annual Professor Singer Memorial Lecture
Events on 06/07/2016
06/07/2016
Satellite Collision Awareness and Avoidance
Spacecraft formation and cluster flight control have seen growing interest in the last decade. However, the problem of finding the optimal debris collision avoidance maneuver for a member of a...
Events on 11/07/2016
11/07/2016
On the conversion of Gas Turbine Combustors – Low Swirl Injection
The research work will discuss investigations into the characteristics of Low Swirl Injector (LSI) technique as a viable modification to be used in the conversion of liquid fuelled aero-engines to...
Events on 13/07/2016
13/07/2016
Thermodynamic Simulation of a Continuous Closed Loop Heated Micro-Turbine Test Facility
This incremental development project is focused around a versatile continuously-running high-speed micro gas turbine research facility, which is capable of matching full engine similarity conditions including pressure loading (synonymous with...
Events on 20/07/2016
20/07/2016
A Low-Cost Laser-Range-Measurement Based Terrain-Following Concept and Error Analysis
This seminar addresses the design and error assessment and analysis of a low cost terrain following system for UAVs. Such a system enables an aircraft to maintain a pre-defined vertical...
Events on 27/07/2016
27/07/2016
Negotiation Between Dynamical Systems with Connectivity Constraints
Multi-agent systems (MAS) have been an important area of study over the past few years. This research will propose a real time sub-optimal solution for an agreement problem in multi-agent...
Events on 03/08/2016
03/08/2016
Micro-Turbojet to Turbofan Conversion via Continuously Variable Transmission: Thermodynamic Performance Study
In this study, the viability, performance, and characteristics of a turbojet-to-turbofan conversion through the use of a continuously variable transmission (CVT) are investigated. By an in-house thermodynamic simulation code, the...
  • Today
  • Event
For more info
Please fill in the details

"*" indicates required fields

This field is for validation purposes and should be left unchanged.
Consent
*required fields are marked with an asterisk
© All rights reserved to Faculty of Aerospace Engineering
Web Development Web Development