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הפקולטה |להנדסת אוירונוטיקה וחלל

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הנדסת אוירונוטיקה וחלל

אודות| הפקולטה

הפקולטה להנדסת אווירונוטיקה וחלל בטכניון ע"ש סטיבן ב. קליין היא מרכז אקדמי ברמה עולמית לאוירונוטיקה ואסטרונאוטיקה, המוקדש ליצירה, הרחבה והפצה של רעיונות וידע במדעי התעופה והחלל.
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להיות חלק |מעתיד התעופה והחלל

חדשות
הטכניון משיק פרס בין-לאומי לחדשנות פורצת דרך בתחומי האווירונוטיקה והחלל
12.08.2026

הטכניון משיק פרס בין-לאומי לחדשנות פורצת דרך בתחומי האווירונוטיקה והחלל

פרס מקס ודזירה בלנקפלד לחדשנות פורצת דרך באווירונוטיקה. הפרס החדש יוקיר תרומות פורצות דרך בהנדסת אווירונוטיקה וחלל ויטפח שיתופי פעולה בין-לאומיים ארוכי טווח וחילופי ידע אקדמי.
קרא עוד
פרופ' משה אידן הועלה לדרגת פרופסור מן המניין
11.08.2026

פרופ' משה אידן הועלה לדרגת פרופסור מן המניין

פרופ' אידן הוא חוקר בעל הכרה בינלאומית, אשר מחקריו תרמו תרומה משמעותית לתחומי תורת השערוך, מערכות בקרת טיסה וניהול התעבורה האווירית.
קרא עוד
פרופסור אלי ליבנה זכה בפרס חנין הבינלאומי לשנת 2026
08.02.2026

פרופסור אלי ליבנה זכה בפרס חנין הבינלאומי לשנת 2026

הפרס הבינלאומי ע"ש פרופ' מאיר חנין ז"ל מוענק מדי שנתיים על הישגים מדעיים וטכנולוגיים משמעותיים במדעי התעופה והחלל.
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כל החדשות
סמינרים
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.
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כל הסמינרים
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Geometric Analysis and Optimization of Doppler-Based Navigation with Low Earth Orbit Satellites
04/05/2026
Geometric Analysis and Optimization of Doppler-Based Navigation with Low Earth Orbit Satellites
Carlos Caravaca Gallego | This work is towards a Ph.D. degree under the supervision of Prof. Pini Gurfiland and Dr. Hector Rotstein
Colloquium: Optimal Guidance under Constraints: Analytical and Numerical Approaches for Missile and Space Applications
11/05/2026
Colloquium: Optimal Guidance under Constraints: Analytical and Numerical Approaches for Missile and Space Applications
Assoc. Prof. Vitaly Shaferman | Optimal guidance under constraints is essential in many aerospace applications, as real-world missions must adhere to strict physical, safety, and operational limitations, such as control bounds, collision-avoidance requirements, and terminal accuracy, while simultaneously achieving high performance, for example, by minimizing fuel consumption or aerodynamic drag.
SPOTLIGHT on RAFAEL
13/05/2026
SPOTLIGHT on RAFAEL
Resilient Decision-Making for Multi-Robot Systems in the Presence of Adversaries
13/05/2026
Resilient Decision-Making for Multi-Robot Systems in the Presence of Adversaries
Roee M. Francos | This talk presents a unified perspective on resilient decision-making for multi-robot systems in environments where adversaries may influence routing, search, and detection tasks. Recently, significant progress in coordination, control, and navigation of multi-robot systems has been achieved, driven primarily by the rapid commercialization of unmanned aerial systems and drones. Yet, real-world deployment remains challenging.
Measuring and Predicting of Vibro-Acoustic Response of a Flat Plate
18/05/2026
Measuring and Predicting of Vibro-Acoustic Response of a Flat Plate
Maayan Naschletashvili | This seminar examines how turbulent airflow excites structural vibrations and, in turn, generates noise transmitted into enclosed spaces. An anechoic wind tunnel experiment was conducted to investigate the vibro-acoustic response of a thin square plate subjected to a turbulent boundary layer.
Research Day 2026
20/05/2026
Research Day 2026
Impact of Aerodynamic Modeling on Aeroelastic Simulations of Straight and Swept wings
25/05/2026
Impact of Aerodynamic Modeling on Aeroelastic Simulations of Straight and Swept wings
Suryapratap Shinde | Highly flexible wings exhibit strong aeroelastic coupling, and the accuracy of static load and deformation predictions depends critically on the fidelity of the aerodynamic model. This research investigates the static aeroelastic behaviour of the Pazy wing using three aerodynamic models of increasing fidelity, all coupled to the same linear elastic modal structural framework.
Semianalytical Orbit Propagation Using Fourier Series Expansions
01/06/2026
Semianalytical Orbit Propagation Using Fourier Series Expansions
Nadav Mailhot | Although satellite orbit propagation is one of the oldest problems in artificial satellite theory, there are still remaining challenges related to propagation speed and precision. In this talk, a new semianalytical orbit propagation method is designed to account for conservative perturbing forces
Colloquium: Phononic crystals for passive hypersonic flow control
03/06/2026
Colloquium: Phononic crystals for passive hypersonic flow control
Pavel Galich | B.Sc. and M.Sc. in Applied Mathematics and Physics, Department of Aerophysics and Space Research, Moscow Institute of Physics and Technology (2012 and 2014). Ph.D. in Aerospace Engineering, Technion (2018). Postdoctoral Research Associate, Department of Materials Science; NanoEngineering (MSNE), Rice University (2018-2020). Assistant Professor at the Technion since 2020.
Events on 04/05/2026
04/05/2026
Geometric Analysis and Optimization of Doppler-Based Navigation with Low Earth Orbit Satellites
Carlos Caravaca Gallego | This work is towards a Ph.D. degree under the supervision of Prof. Pini Gurfiland and Dr. Hector Rotstein
Events on 11/05/2026
11/05/2026
Colloquium: Optimal Guidance under Constraints: Analytical and Numerical Approaches for Missile and Space Applications
Assoc. Prof. Vitaly Shaferman | Optimal guidance under constraints is essential in many aerospace applications, as real-world missions must adhere to strict physical, safety, and operational limitations, such as control bounds, collision-avoidance requirements, and terminal accuracy, while simultaneously achieving high performance, for example, by minimizing fuel consumption or aerodynamic drag.
Events on 13/05/2026
13/05/2026
SPOTLIGHT on RAFAEL
13/05/2026
Resilient Decision-Making for Multi-Robot Systems in the Presence of Adversaries
Roee M. Francos | This talk presents a unified perspective on resilient decision-making for multi-robot systems in environments where adversaries may influence routing, search, and detection tasks. Recently, significant progress in coordination, control, and navigation of multi-robot systems has been achieved, driven primarily by the rapid commercialization of unmanned aerial systems and drones. Yet, real-world deployment remains challenging.
Events on 18/05/2026
18/05/2026
Measuring and Predicting of Vibro-Acoustic Response of a Flat Plate
Maayan Naschletashvili | This seminar examines how turbulent airflow excites structural vibrations and, in turn, generates noise transmitted into enclosed spaces. An anechoic wind tunnel experiment was conducted to investigate the vibro-acoustic response of a thin square plate subjected to a turbulent boundary layer.
Events on 20/05/2026
20/05/2026
Research Day 2026
Events on 25/05/2026
25/05/2026
Impact of Aerodynamic Modeling on Aeroelastic Simulations of Straight and Swept wings
Suryapratap Shinde | Highly flexible wings exhibit strong aeroelastic coupling, and the accuracy of static load and deformation predictions depends critically on the fidelity of the aerodynamic model. This research investigates the static aeroelastic behaviour of the Pazy wing using three aerodynamic models of increasing fidelity, all coupled to the same linear elastic modal structural framework.
Events on 01/06/2026
01/06/2026
Semianalytical Orbit Propagation Using Fourier Series Expansions
Nadav Mailhot | Although satellite orbit propagation is one of the oldest problems in artificial satellite theory, there are still remaining challenges related to propagation speed and precision. In this talk, a new semianalytical orbit propagation method is designed to account for conservative perturbing forces
Events on 03/06/2026
03/06/2026
Colloquium: Phononic crystals for passive hypersonic flow control
Pavel Galich | B.Sc. and M.Sc. in Applied Mathematics and Physics, Department of Aerophysics and Space Research, Moscow Institute of Physics and Technology (2012 and 2014). Ph.D. in Aerospace Engineering, Technion (2018). Postdoctoral Research Associate, Department of Materials Science; NanoEngineering (MSNE), Rice University (2018-2020). Assistant Professor at the Technion since 2020.
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