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
Seminars
November 16 2026
Radar target classification using RCS characteristics
Eliezer Azoulai | This study investigates the feasibility of classifying anti-tank threats, specifically Rocket-Propelled Grenades (RPGs) and Anti-Tank Guided Missiles (ATGMs), based only on their Radar Cross Section (RCS) characteristics. A comprehensive target RCS database was constructed using electromagnetic simulations, and radar tracking scenarios were simulated to generate dynamic RCS measurements under varying Signal-to-Noise Ratio (SNR) levels and carrier frequencies of 10, 20, and 40 GHz.
Read more
All Seminars
Today
Sun
Mon
Tue
Wed
Thu
Fri
Sat
S
M
T
W
T
F
S
27
28
29
30
31
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
Neighboring Extremal Path Applications for Rocket Trajectory Shaping
30/12/2020
Neighboring Extremal Path Applications for Rocket Trajectory Shaping
A guided rocket system performance is often evaluated by solving an optimal control problem which minimizes a pre-defined objective function, e.g. control effort, while satisfying required boundary conditions. However, rocket...
Finding the Worst-Case Behavior of an Accelerating Rocket due to Side-Wind Disturbances
06/01/2021
Finding the Worst-Case Behavior of an Accelerating Rocket due to Side-Wind Disturbances
Flight control law clearance provides the conditions needed for the system to operate in the stability boundaries. One way to do so is to test all the parameters and variables...
Year End Ceremony & Party
07/01/2021
Year End Ceremony & Party
Graduation ceremony and year-end partyץ Class of 2019-2020
Simulation of the Dynamic Response of Aero-Servo-Elastic Wind-Tunnel Model to Non-Uniform Gust
11/01/2021
Simulation of the Dynamic Response of Aero-Servo-Elastic Wind-Tunnel Model to Non-Uniform Gust
Simulation of dynamic response of Aero-Servo-Elastic Wind-Tunnel model to Non-Uniform gust was conducted. The research is done under the “Gust Load Alleviation techniques assessment on wind tunnel Model of advanced...
Fluid-Structure Interactions with Flapping, Compliant Membrane Wings
18/01/2021
Fluid-Structure Interactions with Flapping, Compliant Membrane Wings
Numerous animals including fish, birds, bats and insects use appendages (fins and wings) with varying levels of flexibility, to provide propulsion and/or weight support as they move through either air...
Construction of Non-Equilibrium Hydrodynamic Models for Atmospheric Entry Plasmas
27/01/2021
Construction of Non-Equilibrium Hydrodynamic Models for Atmospheric Entry Plasmas
The simulation of the aerothermal environment surrounding vehicles moving at hypersonic speed is a complex problem due to its multi-physics and multi-scale nature. Progress in the ability to accurately model...
A Preliminary Design Tool for Optimal Effusion Cooling Holes Diameter and Spacing
03/02/2021
A Preliminary Design Tool for Optimal Effusion Cooling Holes Diameter and Spacing
Micro gas turbines generally employ uncooled turbine blades and their thrust is limited by the maximum allowable gas temperature. A miniature cooling scheme embodying effusion cooling may significantly enable higher...
Events on 30/12/2020
30/12/2020
Neighboring Extremal Path Applications for Rocket Trajectory Shaping
A guided rocket system performance is often evaluated by solving an optimal control problem which minimizes a pre-defined objective function, e.g. control effort, while satisfying required boundary conditions. However, rocket...
Events on 06/01/2021
06/01/2021
Finding the Worst-Case Behavior of an Accelerating Rocket due to Side-Wind Disturbances
Flight control law clearance provides the conditions needed for the system to operate in the stability boundaries. One way to do so is to test all the parameters and variables...
Events on 07/01/2021
07/01/2021
Year End Ceremony & Party
Graduation ceremony and year-end partyץ Class of 2019-2020
Events on 11/01/2021
11/01/2021
Simulation of the Dynamic Response of Aero-Servo-Elastic Wind-Tunnel Model to Non-Uniform Gust
Simulation of dynamic response of Aero-Servo-Elastic Wind-Tunnel model to Non-Uniform gust was conducted. The research is done under the “Gust Load Alleviation techniques assessment on wind tunnel Model of advanced...
Events on 18/01/2021
18/01/2021
Fluid-Structure Interactions with Flapping, Compliant Membrane Wings
Numerous animals including fish, birds, bats and insects use appendages (fins and wings) with varying levels of flexibility, to provide propulsion and/or weight support as they move through either air...
Events on 27/01/2021
27/01/2021
Construction of Non-Equilibrium Hydrodynamic Models for Atmospheric Entry Plasmas
The simulation of the aerothermal environment surrounding vehicles moving at hypersonic speed is a complex problem due to its multi-physics and multi-scale nature. Progress in the ability to accurately model...
Events on 03/02/2021
03/02/2021
A Preliminary Design Tool for Optimal Effusion Cooling Holes Diameter and Spacing
Micro gas turbines generally employ uncooled turbine blades and their thrust is limited by the maximum allowable gas temperature. A miniature cooling scheme embodying effusion cooling may significantly enable higher...
  • 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