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Aerospace Engineering

  • Inicio

    Director

     

    Prof. Manuel Soler Arnedo

     

     

    About the program

     

    This Ph.D. gives response to the need for specific training and research in the field of Aerospace Engineering. The main objective of the program is to qualify students with a series of technical and scientific competences in the field of aerospace science and technologies. Graduate doctors of the program will be qualified to find innovative and disruptive solutions to high-impact and high-interest problems in the field of aerospace engineering through a combination of experimental, computational, and technological methodologies pertaining to  aerospace science and engineering with a marked multidisciplinary, intersectoral and international character.

    The program is structured in two large areas:

      Aeronautics

      Space

    Career opportunities for graduates are focused on three areas: a scientific career in universities or national and international research centers; a professional career in the Aerospace R&D sector; and the creation of technology-based companies through patents and/or registered software as direct outcomes of the research.

     

    • Programa adaptado al Real Decreto 99/2011, de 28 de enero
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    Departament

    Department of Aerospace Engineering

    (María de Maeztu Unit of Excellence)

    For further information:

    Please visit the Aerospace Engineering website

    Ingenieria Aeroespacial Doctorado UC3M
  • ACCESS

    Student profile

    The program considers as a recommended access profile a graduate background training in the field of Science, Engineering and Architecture and, specifically, the area of the program, Aerospace Engineering.

    The program is open to students with Master's degrees in the areas of Manufacturing Engineering, Systems Engineering and Automation, Electrical Engineering, Mechanical Engineering, Mathematics, Thermal Engines and Machines, Fluid Mechanics, Continuum Mechanics and Structural Analysis, Applied Physics, Chemical Engineering, Telematic Engineering, Electronic Technology or Signal Theory and Communications. In these cases, some graduate training in the specific areas of the program is required. The Academic Committee will determine the complementary research training that candidates need according to their particular background.

    The UC3M Master's degrees with direct access to the Ph.D. are the Master in Aeronautical Engineering (MAE), the  Master in Space Engineering (MISE), and the Master in Aerospace Science and Technology (MAST)

    Access requirements

    According to art. 6 of the PhD studies regulation (RD 99/2011), in order to access the Program it is required to have a Bachelor's degree (or equivalent) and a Master's degree (or equivalent), provided that at least 300 ECTS credits have been passed in these two cycles as a whole, or the equivalent degree qualifies for level 3 of MECES (Marco Español de Cualificaciones para la Educación Superior, Spanish Framework for Higher Education Qualifications).

    Likewise, access is available to candidates in possession of foreign degrees from countries integrated into the European Higher Education Area (EHEA) when the degree can be accredited as level 7 in the European Qualifications Framework (EQF), as long as the aforementioned degree allows access to PhD level studies in the country of expedition; and candidates with a degree which is equivalent to a Spanish Master's degree, obtained in foreign education systems outside the EHEA, as long as the aforementioned degree allows access to PhD level studies in the country of expedition.

    Students with graduate training in areas other than the Aerospace Engineering can be also admitted. These students shall have Master-level training in: 

    • Science (Mathematics or Applied Physics)
    • Engineering and Architecture: Manufacturing Engineering, Systems Engineering and Automation, Electrical Engineering, Mechanical Engineering, Thermal Engines and Machines, Fluid Mechanics, Continuum Mechanics and Structural Analysis, Chemical Engineering, Telematic Engineering, Electronic Technology or Signal Theory and Communications.

    Admission criteria

     

    Admission is based on the criteria established by the Academic Committee listed below. These are implemented by the director of the program, who reports to the Committee on a regular basis. 

    In the admission and selection process, the Academic Committee will consider:

    • Academic transcript (Bachelor's and Master's degrees). Formulas from competitive programs such as FPU (Formación de Profesorado Universitario, a Ph.D. scholarship program at national level in Spain) will be used to quantify the grade, including equivalence from non-Spanish transcripts. Weight: 60%.
    • Suitability of the candidate's background training (subjects, grades and language skills) to the lines of research of the Ph.D. program. Weight: 20%.
    • Research experience (publications, conferences, etc.). Weight: 15%.
    • Motivation, commitment to the program and research interests of the candidate, all of which will be assessed based on a motivation letter. The candidate can provide one or more endorsement letters from a researcher from any university, which will serve as proof of commitment. Weight: 5%.

    The Academic Committee can require a personal interview with the candidate. This will not be considered as part of the admission criteria with a specific weight but, rather, an additional tool for clarification of the suitability and motivation of the student.

     

    In their admission resolution, the Academic Committee, considering the certified training of the candidate, can establish some complementary training based on the following criteria:

    Access profile Complementary training
    Students with a Master's degree in the field of Aerospace Engineering or a minimum 60 ECTS. Not required
    Students with a Master's degree in the field of Engineering and Architecture: Manufacturing Engineering, Systems Engineering and Automation, Electrical Engineering, Mechanical Engineering, Thermal Engines and Machines, Fluid Mechanics, Continuum Mechanics and Structural Analysis, Chemical Engineering, Telematic Engineering, Electronic Technology or Signal Theory and Communications, with a minimum 60 ECTS. Up to 18 ECTS in the field of Aerospace Engineering
    Students with a Master's degree in the field of Science (Mathematics or Applied Physics), with a minimum 60 ECTS Up to 30 ECTS in the field of Aerospace Engineering

     

    As a general rule, for students with no training or experience in research methodology,the Academic Committee can establish complementary training consisting in either subjects of a Master's degree in the field of Aerospace Engineering or a supervised research work that qualifies the student with knowledge in research methods and public presentation skills before an evaluating committee.

     

    Seats available for the current academic year: 8

     

  • FACULTY
  • TRAINING

    Concurrently with the doctoral thesis work, Ph.D. candidates must follow a training program to improve their research skills and ensure the scientific quality of their research work. This program is structured on the following training elements.

     

    Specific training

     

    • Doctoral meetings

    Workshop-format sessions in which Ph.D. candidates present the state of their research, followed by a period for discussion and questions from the audience. These meetings are attended by other Ph.D. candidates, their tutors or advisors, and other university professors from the program. If a research work is in the process of registration or protection of intellectual property, the tutor or advisor can request from the Academic Committee a restriction on the disclosure of information until the resolution of the process. 

    This activity is mandatory: 10 hours per academic year (including the 4 hours of session attendance) throughout the doctoral training period. These meetings take place on an annual basis, at the least.

    For evaluation purposes, the Ph.D. candidate will provide proof of attendance and a report supervised by the thesis advisor detailing the conclusions and possible impact of the discussion on their research project. 

     

    • Conferences or presentations by the PhD candidate​

    The Ph.D. candidate must give at least one conference or presentation in front of a qualified audience (e. g., a congress or masterclass). Students who cannot attend these forums can do these presentations in the context of the abovementioned doctoral meetings as an additional activity. 

    ​​This activity is mandatory: 10 hours (9 hours of preparation and 1 hour of presentation) throughout the doctoral training period.

    For evaluation purposes, the Ph.D. candidate will provide proof of attendance and a report supervised by the thesis advisor detailing the conclusions and possible impact of the discussion on their research project. 

     

    • Scientific articles

    The Ph.D. candidate must write, submit and have published (or, in lack thereof, provide a letter of acceptance from the editor) at least one Web of Science-indexed paper.

    This activity is mandatory: 100 hours, including writing and review, throughout the doctoral training period.

    The scientific article itself, which must have been subject to a peer review process, will be considered for evaluation purposes.

     

    • Specific seminars

    Seminars of variable duration hosted by either this Ph.D. program or others from the Escuela Politécnica Superior, or by departments, academic units, university institutes, research institutes or other universities or research centers (national or regional). These seminars are conducted in English (as a general rule) or Spanish. Students will choose the seminars according to their research interests.

    This activity is optional. However, the Academic Committee of the program may require 20 to 40 hours of this activity (incuding 8 to 16 hours of attendance) throughout the doctoral training period, according to the training and former research or career experience of the Ph.D. candidate.

    For evaluation purposes, the Ph.D. candidate will provide proof of attendance and a supervised critique report supervised by the thesis advisor on the contents of the seminar in relation to the research topic of the Ph.D. candidate. The Academic Committee will have authority to validate seminars hosted by institutions other than UC3M.

     

    • Research visits in centers of national or international reference

    The program promotes the mobility of students with training activities in research centers of reference with Ph.D. programs of proven quality in Spain and abroad.

    This activity is optional. The duration of the visit must be one month at least. This activity can qualify as a requirement for the Doctorado Internacional distinction, provided that it is carried out at a center outside Spain and that the duration is of at least three months. 

    Ph.D. candidates can do this activity troughout their entire doctoral period training and choose the dates according to their interests. However, it is recommended to carry it out during the second or third doctoral year.

    Ph.D. candidates can attend courses and seminars organized by the host institution during the visit. This training can be considered as one of the requirements of the abovementioned activities (specific seminars, specialized courses, etc.).

    For evaluation purposes, the Ph.D. candidate will provide proof of completion from the host institution and a report on the activities, courses and seminars, as well as the progress on the thesis research made during the visit.

     

     

    Research skills training

     

    Optional. Up to 2 credits throughout the doctoral training period.

    Research skills training is focused on abilities common to all disciplines for the development of scientific and educational skills and the improvement of the professional career. This training consists of different activities (short courses, seminars, etc.), which can be recommended by the Academic Committee of the program.

     

    Further information:

     

  • RESEARCH
    • Lines of research

      AERONAUTICS

       

      Aerospace structures and materials​

      • Aeronautical structures
      • Composites and advanced materials.
      • Structural health monitoring
      • Structural dynamics and vibroacoustics
      • Aeroelasticity

      Air Navigation and Control​

      • Commercial Aircraft Trajectory Optimization
      • Meteorological Uncertainty Management
      • Aviation Induced Environmental Impact
      • Artificial Intelligence Applications to Air Traffic Management
      • Unmanned Air Vehicles (UAVs)

      Aerospace Design and Manufacturing​

      •  Optimization and multidisciplinary design
      •  Non-conventional aircraft
      •  Manufacturing processes
      • Airborne wind energy systems 

      Aerodynamics​ and Propulsion

      • External aerodynamics
      • Turbulence
      • Internal flows and propulsion
      • Experimental techniques
      • Computational techniques

       

       

      SPACE

       

      Propulsion and Space Environment​

      • Plasma engines
      • Magnetic nozzles
      • Radiofrecuency and microwaves sources
      • Plasma-spaceship interaction
      • Space Debris Removal
      • Plasma waves and ECR motors
      • Plasma diagnosis

      Astrodynamics

      • Space Tethers
      • Mission analysis and trajectory optimization
      • Orbit Determination and Space Surveillance and Tracking

      Space Systems

      • Satellite Design and Systems Engineering
      • Subsystems design
      • Onboard software
      • Communications
      • Space Electronics
      • Space automation
      • Scientific Instrumentation
    • Scientific results

      Publications from the doctoral theses defended in the PhD program

      • Thesis: Emissive Langmuir Probe Theory with Application to Low Work Function Electrodynamic Tethers
        Author: Luca Chiabo
        Publication: Chiabò, L., Shahasavani, S., Sánchez-Arriaga, G. (2021). Kinetic Analysis of the plasma sheath around en electron-emitting object with elliptic cross section. Physical Review E, 104, 055204. DOI: https://doi.org/10.1103/PhysRevE.104.055204
      • Thesis: Aircraft Trajectory Planning Considering Ensemble Forecasting of Thunderstorms
        Author:  Eduardo Andrés Enderiz
        Publication: Andrés, E. González-Arribas, D., Soler, M., Kamgarpour M., Sanjurjo-Rivo, M., Simarro, J. “Iterative graph deformation for aircraft trajectory planning considering ensemble forecasting of thunderstorms”. In: Transportation Research Part C: Emerging Technologies 145 (2022). Doi: https://10.1016/j.trc.2022.103919
      • Thesis: Unsteady Aerodynamics of Delta Kites applied to Airborne Wind Energy Systems
        Author:  Iván Castro Fernández
        Publication: Castro-Fernández,I., DeLosRíos-Navarrete, F., Borobia-Moreno, R., & al. Automatic testbed with a visual motiontracking system for airborne wind energy applications. Wind Energy. 2023;1‐14. Doi: https://10.1002/we.2805
      • Thesis: Fluid-kinetic models for space plasma thrusters
        Author:  Jesús Perales Díaz
        Publication: Perales-Díaz, J., Domínguez-Vázquez, A., Fajardo, P., & Ahedo, E. (2023). Simulations of driven breathing modes of a magnetically shielded Hall thruster. Plasma Sources Science and Technology. Doi: https://iopscience.iop.org/article/10.1088/1361-6595/ace651
      • Thesis: Analysis of Turbulent Transport in Hall-Effect Plasma Thrusters
        Author: Enrique Bello Benitez
        Publication: Bello-Benítez, E., & Ahedo, E. (2023). Stationary axial model of the Hall thruster plasma discharge: electron azimuthal inertia and far plume effects. Plasma Sources Science and Technology, 32(11), 115011. Doi: https://doi.org/10.1088/1361-6595/ad066f
      • Thesis: Two-dimensional model of wall interaction in Hall effect thruster discharges
        Author:  Alberto Marín Cebrián
        Publication: Marín-Cebrián, A., Domínguez-Vázquez, A., Fajardo, P., & Ahedo, E. (2022). Kinetic plasma dynamics in a radial model of a Hall thruster with a curved magnetic field. Plasma Sources Science and Technology. Doi: https://10.1088/1361-6595/ac9a6b
      • Thesis: Low-Reynolds-number aerodynamic effects in unsteady flow environments
        Author:  Juan Manuel Catalán Gómez
        Publication: Paper 1. Catalán, J.M., Olivieri, S., García-Villalba, M. and Flores, O., 2024. On the generation of free-stream turbulence at low Reynolds number: a numerical study. Comput. Fluids. 280, 106345.
      • Thesis: Robust Model Predictive Control for Autonomous Guidance & Control in Space Scenarios
        Author:  Thomas Aleksander Frekhaug
        Publication: Frekhaug, T., Sanjurjo, M., Soler, M., Hudson, J., & Romano, M. (2024), Robust Model Predictive Control for Proximity Operations with Experimental Demonstrations. Journal of Guidance, Control, and Dynamics, DOI: https://doi.org/10.2514/1.G008190
      • Thesis: Robust Aircraft Trajectory Optimization & Climate Change
        Author:  Abolfazl Simorgh
        Publication: Simorgh, A., Soler, M., Castino, F., Yin, F., & Cerezo-Magaña, M. (2024). Concept of robust climate-friendly flight planning under multiple climate impact estimates. Transportation Research Part D: Transport and Environment, 131, 104215. DOI: https://doi.org/10.1016/j.trd.2024.104215
      • Thesis: Perturbed-Analytic Direct transcription for Optimal Control (PADOC) with Application in Commercial Aircraft Trajectory Optimization
        Author:  Amin Jafarimoghaddam
        Publication: Jafarimoghaddam, A., Soler, M. “Perturbed-analytic direct transcription for optimal control (PADOC)”. Optimal Control Applications and Methods. 2023. Doi: https://doi.org/10.1002/oca.2965
    • Scientific publications

      AERONAUTICS

      Aeronautical structures and materials​

      • Vanesa Guerrero Lozano, “A mathematical optimization approach to shape-constrained generalized additive models” (2024) Rev. Expert Systems with Applications. Vol. 255. Pág. 124654-1 – 124654-16. ISSN: 0957-4174. JCR: 7,5. SCOPUS: 1,875. DOI: https://doi.org/10.1016/j.eswa.2024.124654
      • Andrea Cini, “Analytical fatigue life formulation for notches informed by crystal plasticity” (2022) Rev. International Journal of Fatigue. Vol. 163. Pág. 107072-1 – 107072-11. ISSN: 0142-1123. JCR: 5,7. SCOPUS: 1,528. DOI: https://doi.org/10.1016/j.ijfatigue.2022.107072

      Air navigation and Control

      • Manuel Fernando Soler Arnedo, “Perturbed-analytic direct transcription for optimal control (PADOC)” (2023) Rev. Optimal Control Applications and Methods. Vol. 44. DOI: https://doi.org/10.1002/oca.2965
      • Manuel Fernando Soler Arnedo, “Concept of robust climate-friendly flight planning under multiple climate impact estimates” (2024) Rev. Transportation Research Part D-Transport and Enviroment. Vol. 131. Pág. 104215-1 – 104215-23. ISSN: 1361-9209. JCR: 7,4. SCOPUS: 2,328. DOI: https://doi.org/10.1016/j.trd.2024.104215
      • Manuel Fernando Soler Arnedo, Manuel Sanjurjo Rivo, “Informed scenario-based RRT* for aircraft trajectory planning under ensemble forecasting of thunderstorms” (2021) Rev. Transportation Research Part C-Emerging Technologies. Vol. 129. Pág. 103232 – 103253. ISSN: 0968-090X. JCR: 7,6. SCOPUS: 2,86. DOI: https://doi.org/10.1016/j.trc.2021.103232
      • Andrés Marcos Esteban, “Design of Structured  H-infinity flight controllers: Passive fault-tolerant versus observer-based structures” (2023) Rev. ISA Transactions. Vol. 143. Pág. 20-37. ISSN: 0019-0578. JCR: 6,3. SCOPUS: 1,572. DOI: https://doi.org/10.1016/j.isatra.2023.08.029
      • Andrés Marcos Esteban, “The VEGA launcher atmospheric control problem: a case for linear parameter-varying synthesis” (2022) Rev. Journal of the Franklin Institute – Engineering and Applied Mathematics. Vol. 359. Pág. 899-927. ISSN: 0016-0032. JCR: 3,7. SCOPUS: 1,191. DOI: https://doi.org/10.1016/j.jfranklin.2021.07.057

      Aeronautical design and manufacturing

      • Rauno Cavallaro, Gonzalo Sánchez Arriaga, “Automatic testbed with a visual motion tracking system for airborne wind energy applications” (2023) Rev. Wind Energy. ISSN: 1095-4244. JCR: 4, SCOPUS: 1,128. DOI: https://doi.org/10.1002/we.2805
      • Gonzalo Sánchez Arriaga, “Identification of kite aerodynamic characteristics using the estimation before modeling technique” (2021) Rev. Wind Energy. Vol. 24. Pág. 596-608. ISSN: 1095-4244. JCR: 4, SCOPUS: 1,128. DOI: https://doi.org/10.1002/we.2591
      • Rauno Cavallaro, Gonzalo Sánchez Arriaga, “Automatic testbed with a visual motion tracking system for airborne wind energy applications” (2023) Rev. Wind Energy. ISSN: 1095-4244. JCR: 4, SCOPUS: 1,128. DOI: https://doi.org/10.1002/we.2805

      Aerodynamics and Propulsion

      • Stefano Discetti, Carlos Sanmiguel Vila, “Super-resolution generative adversarial networks of randomly-seeded fields” (2022) Rev. Nature Machine Intelligence. Vol. 4. Pág. 1165-1173. ISSN: 2522-5839. JCR: 18,8. SCOPUS: 5,94. DOI: https://doi.org/10.1038/s42256-022-00572-7
      • Andrea Ianiro, Stefano Discetti, Rodrigo Castellanos García de Blas, Marco Raiola, “Heat transfer enhancement in turbulent boundary layers with a pulsed slot jet in crossflow” (2023). Rev. Applied Thermal Engineering. Vol. 219, Part. C. Pág. 1-14. JCR: 6,1. SCOPUS: 1,488. DOI: https://doi.org/10.1016/j.applthermaleng.2022.119595

      SPACE

      Propulsion and space environment

      • Eduardo Ahedo Galilea, Pablo Fajardo Peña, Adrian Dominguez Vazquez, “Simulations of driven breathing modes of a magnetically shielded Hall thruster” (2023) Rev. Plasma Sources Science & Technology. Vol. 32. Pág. 1-19. ISSN: 0963-0252. JCR: 3,3. SCOPUS: 0,771. DOI: https://doi.org/10.1088/1361-6595/ace651
      • Eduardo Ahedo Galilea, Adrian Dominguez Vazquez, “Non-Maxwellian electron effects on the macroscopic response of a Hall thruster discharge from an axial&-radial kinetic model” (2024) Rev. Plasma Sources Science & Technology. Vol. 33. Pág. 025008-1 – 025008-20. ISSN: 0963-0252. JCR: 3,3. SCOPUS: 0,771. DOI: https://doi.org/10.1088/1361-6595/ad227c
      • Jaume Navarro Cavalle, Pablo Fajardo Peña, “Mechanically Amplified Milli-Newton Thrust Balance for Direct Thrust Measurements of Electric Thrusters for Space Propulsion” (2020) Rev. IEEE Transactions on Instrumentation and Measurement. Vol. 70. Pág. 3505318-1 – 3505318-1. ISSN: 0018-9456. JCR: 5,6. SCOPUS: 1,536. DOI: https://doi.org/10.1109/TIM.2020.3037305
      • Mario Merino Martínez, “An implicit, conservative electrostatic particle-in-cell algorithm for paraxial magnetic nozzles” (2024) Rev. Journal of Computational Physics. Vol. 502. Pág. 1-22. ISSN: 0021-9991. JCR: 3,8. SCOPUS: 1,679. DOI: https://doi.org/10.1016/j.jcp.2024.112826
      • Mario Merino Martínez, Eduardo Antonio Ahedo Galilea, “Plasma acceleration in a magnetic arch” (2023) Rev. Plasma Sources Science & Technology. Vol. 32. Pág. 1-12. ISSN: 0963-0252. JCR: 3,3. SCOPUS: 0,771. DOI: https://doi.org/10.1088/1361-6595/acd476

      Astrodynamics

      • Manuel Fernando Soler Arnedo, Manuel Sanjurjo Rivo,“Hybrid multi-objective orbit-raising with operational constraints” (2020) Rev. Acta Astronautica. Vol. 175. Pág. 447-461. ISSN: 0094-5765. JCR: 3,1. SCOPUS: 1,106. DOI: https://doi.org/10.1016/j.actaastro.2020.05.022
      • Joaquín Miguez Arenas, “A likely magnetic activity cycle for the Exoplanet Host M Dwarf GJ 3512” (2020) Rev. Astronomical Journal. Vol. 160. Pág. 273. ISSN: 0004-6256. JCR: 5,1. SCOPUS: 1,953. DOI: https://doi.org/10.3847/1538-3881/abc171

      Space systems

      • Guillermo Carpintero Del Barrio, “Integrated dual-laser photonic chip for high-purity carrier generation enabling ultrafast terahertz wireless communications” (2022) Rev. Nature Communications. ISSN: 2041-1723. JCR: 14,7. SCOPUS: 4,887. DOI: https://10.1038/s41467-022-29049-2
      • Gonzalo Sánchez Arriaga, “The effect of cesium dopant on APCVD graphene coating on copper” (2020) Rev. Journal of Materials Research and Technology-JMR&T. Vol. 9. Pág. 9798-9812. ISSN: 2238-7854. JCR: 6,2. SCOPUS: 1,091. DOI: https://doi.org/10.1016/j.jmrt.2020.06.091
      • Gonzalo Sánchez Arriaga, “Limitations of stationary Vlasov-Poisson solvers in probe theory” (2021) Rev. Journal of Computational Physics. Vol. 438. Pág. 1-13. ISSN: 0021-9991. JCR: 3,8. SCOPUS: 1,679. DOI: https://doi.org/10.1016/j.jcp.2021.110366
  • THESIS

    Preparation of the thesis

    Please check the Guide with recommendations that the University Library has accessible on its website.

    You must always follow the guidelines of your thesis advisor, the guidelines of your doctoral program, and the regulations of the Doctoral School.

    Thesis defense

    The doctoral thesis consists of an original research work developed by the Ph.D. candidate in the field of knowledge established by the program. It enables the student for autonomous work in the field of R+D+i.

    Universidad Carlos III de Madrid and its Doctoral School establish follow-up procedures to guarantee the quality of the student's training and supervision. They also facilitate the procedures for the proper evaluation and defense of the doctoral thesis.

    Further information:

    Compendium of publications

    The Academic Committee for the PhD Program may authorize the presentation fo a thesis in the modality "compendium of publication", according to the information established in the following document Tesis por compendio de publicaciones Ing. Aeroespacial

    Requirements for thesis defense in Aerospace Engineering

    Except for some special cases, students must have published (or, in lack thereof, have a letter of acceptance from the editor) at least one Web Of Science-indexed paper in order to be evaluated by the Academic Committee of the Program.

  • QUALITY

    GENERAL INFORMATION ABOUT PH.D.

    Implementation Year: 2020-2021

    QUALITY ASSURANCE

    The Academic Committee of the Ph.D. complies with the SGIC of Universidad Carlos III de Madrid  . It is responsible for the quality analysis of the program and produces the Degree Reports ("Memoria Académica de Titulación").

    • Academic Committee
    • Reports from the Quality Assurance Committee (Restricted access) (Available soon)

    QUALITY INDICATORS 

    COMPLAINTS AND SUGGESTIONS

  • CONTACT
    Bienvenida Universidad Carlos III de Madrid

    Doctoral School Office | Leganés Campus

    Rey Pastor Building, Office 3.0.B.08
    Avenida de la Universidad, 30
    28911 Leganés (Madrid)

    Contact