Contact Us

THE STEPHEN B. KLEIN FACULTY OF |AEROSPACE ENGINEERING

Propelling the Future

Research Labs

REGISTER to IACAS 2026

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.

BE PART OF THE |AEROSPACE FUTURE

News
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.
01.01.2026

Announcing the appointment of the new Dean, Prof. Gil Iosilevskii

The Stephen B. Klein Faculty of Aerospace Engineering is pleased to announce a leadership transition.
12.11.2025

Professor Emeritus Dan Givoli has been selected as the 2026 Timoshenko Scholar at Stanford University

The Timoshenko Scholar is a prestigious award presented annually in recognition of outstanding contributions to the field of applied mechanics.
Events
March 25 2026
RAFAEL will present their Aerospace related activities.
April 29 2026
AE Rocks! Super-talented faculty members and students will play and sing at the 6th Annual Faculty Concert.
May 20 2026
The students’ annual event
Seminars
February 09 2026
Amit Sigawi earned his B.Sc. (cum laude) from the Aerospace Engineering Faculty in 2022, as part of the Silon excellence program. Serves as an engineer in the Air Force since then.
February 11 2026
Kirill Reznik received his first degree in Mechanical Engineering with a specialization in rocket launch systems from Bauman Moscow State Technical University. He is currently completing his MSc in Aerospace Engineering at the Technion, where his research focuses on cooperative missile guidance under the supervision of Prof. Tal Shima.
Sun
Mon
Tue
Wed
Thu
Fri
Sat
S
M
T
W
T
F
S
30
31
1
2
3
4
5
6
8
10
11
12
13
15
17
18
19
20
22
23
24
25
26
27
28
1
2
3
4
5
This work suggests and demonstrates a method for generating reduced chemical kinetic mechanisms for aviation fuels. Small but accurate mechanisms are needed for use in Computational Fluid Dynamics (CFD) combustion...
Hot Wire Anemometry (HWA) methodology has yet to fully realize its potential. As a consequence, nowadays, the use of HWA is unapplicable to flow conditions in the range of 0.4<M<1.2....
Brownian motion, the random motion of particles suspended in a medium, was first studied mathematically by Einstein and Smoluchowski. They obtained the particle's mean square displacement (MSD) in a quiescent...
This talk will present a novel algorithm for early detection of aeroelastic flutter when onset conditions are approached during flutter tests of flight vehicles. The approached stability boundary is detected...
Experimental measurements in actual combustors typically produce measurements that are narrowly relevant to only specific geometries and not easily generalized. Moreover, in experimental studies, relevant mixing scales (e.g., Batchelor scales)...
The research presents a novel approach for propelling high-speed, submerged, marine vehicles. The operating principle is based on the operation of a ram-rocket (ducted-rocket) motor (solid or hybrid), where water...
Events on 07/02/2022
This work suggests and demonstrates a method for generating reduced chemical kinetic mechanisms for aviation fuels. Small but accurate mechanisms are needed for use in Computational Fluid Dynamics (CFD) combustion...
Events on 09/02/2022
Hot Wire Anemometry (HWA) methodology has yet to fully realize its potential. As a consequence, nowadays, the use of HWA is unapplicable to flow conditions in the range of 0.4<M<1.2....
Events on 14/02/2022
Brownian motion, the random motion of particles suspended in a medium, was first studied mathematically by Einstein and Smoluchowski. They obtained the particle's mean square displacement (MSD) in a quiescent...
Events on 16/02/2022
This talk will present a novel algorithm for early detection of aeroelastic flutter when onset conditions are approached during flutter tests of flight vehicles. The approached stability boundary is detected...
Events on 21/02/2022
Experimental measurements in actual combustors typically produce measurements that are narrowly relevant to only specific geometries and not easily generalized. Moreover, in experimental studies, relevant mixing scales (e.g., Batchelor scales)...
Events on 02/03/2022
The research presents a novel approach for propelling high-speed, submerged, marine vehicles. The operating principle is based on the operation of a ram-rocket (ducted-rocket) motor (solid or hybrid), where water...
  • Today
  • Event
For more info
Please fill in the details

"*" indicates required fields

This field is for validation purposes and should be left unchanged.
*required fields are marked with an asterisk