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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.

אנו מחפשים חברי סגל לקידום מחקר והוראה בפקולטה.
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כל מה שצריך לדעת על הקבלה לפקולטה שמציעה את הלימודים הכי גבוהים שיש.

להיות חלק |מעתיד התעופה והחלל

חדשות
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.
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.
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.
סמינרים
October 05 2026
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.
October 14 2026
Bar Gawi | Hypersonic gliding vehicles (HGVs) operate in flight regimes characterized by nonlinear dynamics, significant aerodynamic uncertainties, and strong coupling between vehicle motions. These characteristics pose challenges for flight control design, particularly when tracking performance must be maintained despite model inaccuracies, changing flight conditions, and practical implementation limitations.
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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.
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.
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.
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.
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
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
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
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
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
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 25/05/2026
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
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
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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