MASTER OF SCIENCE IN AEROSPACE ENGINEERING
The Master of Science in Aerospace Engineering programme is awarded by Technische Universität München (Technical University of Munich, TUM). The programme is conducted in Singapore and it serves to provide graduates with an in-depth knowledge in the field of aerospace engineering, focusing in the areas of aeronautical and space design and research.
The 2-year full-time programme Masters in Aerospace Engineering is taught by academia from TUM, who have extensive experience in the latest trends in research and education as well as in global industrial product development and management. The non-technical subjects are taught by experts from the industry, from Asia and Europe alike. Lectures will be held at TUM Asia‘s campus in Singapore.
Students who have passed all examinations and satisfied the criteria to graduate will be awarded a Masters degree from TUM.
“In order to pursue a career in the field of my interest, it was necessary to understand the finer nuances of the subject on hand. This Aerospace Engineering Master degree did so for me.”
Somen Bhudolia (Graduate, MSc in Aerospace Engineering)
DEGREE/FH DIPLOMA* REQUIREMENTS
In order to be eligible for the programme, you must have at least a Bachelor Degree** (completed in at least three years, depending on factors such as the rest of your education background) in Aerospace, Mechanical Engineering, Advanced Mechanics, Mechatronics, Robotics, Avionics, Aircraft Engineering or in a closely related discipline with remarkable results.
*If you meet the requirements for admissions, please refer to this page (Click on “Required Documents”) for the List of Required Documents for application to our Master of Science programmes.
**Academic requirements may differ for different countries of study. Please write to us at email@example.com to verify your requirements.
Submit the Module Descriptions of all the modules you have taken in your Transcript, as found in your curriculum document or syllabus handbook (only applicable for MSc in Aerospace Engineering applications and only required in softcopy format).
ENGLISH LANGUAGE SKILLS
As the Master of Science programme’s instruction medium is English, the applicant must be able to demonstrate a satisfactory level of proficiency in the English language.
Applicant whose native tongue or medium of instruction from previous studies (Bachelor / FH Diploma) is not English must submit at least one of the following:
SPECIAL CRITERIA (China, India & Vietnam)
Additionally, an Akademische Prüfstelle (APS) certificate is required for applicants with education qualifications from China, India or Vietnam. The APS certificate is compulsory if your Bachelor studies was completed in a Chinese, Indian or Vietnamese university, regardless of nationality.
For example, a Singapore citizen who completed his entire undergraduate studies in a Chinese university, and holds a Chinese degree, must sit for the APS test and pass it in order to qualify for admissions to a German university.
If you are making any application to a German university (including the TUM degrees at TUM Asia), the APS certificate is required for all education qualifications from China, India or Vietnam. If you need more information, please contact our team.
More about APS:
IMPORTANT: The provided information is accurate as of AY2023/24 intake and is subject to change.
The teaching faculty in the programme are predominately from TUM, as well as additional modules taught by industry leaders and other expert academics.
Single yearly intake, with course commencement in August every year.
COURSEWORK & STUDENT-TEACHER RATIO
All coursework are conducted in English and students will be taught by German and Singaporean lecturers. Student-teacher ratio averages between 20:1 to 40:1. Only live teaching is conducted in all TUM Asia classes. All examinations will be written by the student him/herself, and examination results are released approximately 1-3 months after the examination.
The Master of Science in Aerospace Engineering degree is a 2-year full-time programme. Students must complete their coursework, 3-month internship and 6-month of Master Thesis writing to qualify for graduation.
In order for a student to graduate from the degree programme, he/she have to complete all 120 ECTS credit with a pass. The regular study duration for this programme is 2 years. The maximum candidature period permitted is 3 years.
All modules carry 5 ECTS Credits each.
This module will provide a basic overview of the different systems and processes applied in aviation. A general understanding of civil and military aviation will be given to enable basic differentiation of different aircraft configurational layouts. In particular, the interaction among different system elements, their respective requirements and their impact on configuration level will be outlined.
Lecturers: Prof. Mirko Hornung / Hours: 45 / Semester: 1
Mechanics addresses the description and predetermination of the movements of bodies and their corresponding forces. Bodies at rest as a sub-field of mechanics are described in (elasto-)statics, the fundamentals of which are taught in this module. After successful participation, students are able to recognize static load-bearing structures in nature and technology and can extract mechanical models from reality, classify them in terms of analysis and calculate statically determinate as well as statically indeterminate systems using the methods they have learned. The basic methods learned contribute to the development of the ability to formulate mechanical issues in engineering problems and to solve them independently.
Lecturers: Prof. Dr. Markus Ryll / Hours: 45 / Semester: 1
Choose a minimum of 3 out of the 4 modules below.
The module Aerodynamics deals with the basics of calculation and analysis of aerodynamic forces acting on aircraft.
Lecturers: Prof. Christian Breitsamter / Hours: 45 / Semester: 1
This module will cover topics in flight system dynamics and flight control. Students will be able to understand relations between aircraft performance and flight control. Through this course, students will be able to apply aircraft performance calculations that are required in the preliminary design of aircraft and will be able to design basic flight controllers for stabilisation and improvement of flight properties.
Lecturers: Prof. Florian Holzapfel / Hours: 45 / Semester: 1
The module provides basic knowledge about aerospace propulsion systems. The basic governing thermodynamic & aerodynamic equations used in the engine design process, Aero engine and gas turbine cycle and component performance as well as their interaction will be covered.
Lecturers: Prof. Volker Gümmer / Hours: 45 / Semester: 1
This module covers the essentials of lightweight structures & materials, which provide a basis for structural development including proper material selection. A general view on the basics in elasticity, structural stability, vibrations and strength including fatigue problems are given. Design, numerical analysis and test methods are introduced. On the materials side, metal lightweight alloys and fiber composites are covered.
Lecturers: Prof. Horst Baier / Hours: 45 / Semester: 1
Choose a minimum of 2 out of the 3 modules below.
This module provides a comprehensive introduction to the functionality of the software MATLAB / Simulink and explains the aerospace engineering problems the tool can be used to solve. Emphasis is placed on numerical modelling of technical problems and the engineering interpretation of results. For dynamic vibration behavior, syntheses will be made with control simulation to show the interaction of several disciplines and to introduce the field of controlling flexible systems to students.
Lecturers: Prof. Florian Holzapfel / Hours: 45 / Semester: 2
The course demonstrates the use of common Finite Element software tools using typical examples from the field of aerospace structures. The most important basics of FEM, and modelling aspects will be covered. Typical questions in the structural calculation from the areas of statics and dynamics serve as examples. With the knowledge gained, aeronautical structures can be modelled, analysed and evaluated with regard to their characteristics.
Lecturers: Andreas Hermanutz / Hours: 45 / Semester: 2
The course provides an introduction to fluid dynamics modelling for aerospace applications. After successful participation, students are able to understand different models and methods available in current flow simulation tools. The set-up and execution of flow simulations as well as the analysis and evaluation of the results are discussed. Upon successful completion, participants will be able to analyse and evaluate aerodynamic properties, such as forces and pressure distributions, as required in the aircraft design process.
Lecturers: Andreas Hermanutz / Hours: 22.5 / Semester: 2
This module conveys complex control concepts for aircraft. How the C*-criterion is derived and modern concepts of adaptive control in aviation are covered.
Lecturer: Prof. Florian Holzapfel / Hours: 45 / Semester: 2-3
This module covers the various types of turbomachinery applications with particular emphasis on compressors. Starting from the fundamental equations in fluid dynamics, the working principle of turbomachinery are derived. Moreover, main components, characteristics and associated flow phenomena are explained. For compressors, design methods and processes, topics of operability and stability enhancement are covered.
Lecturers: Prof. Volker Gümmer / Hours: 45 / Semester: 2-3
This module describes basic aeroelastic phenomena arising from the mutual interaction of elastic, aerodynamic and inertial forces on a structure, with special emphasis on problems related to fixed wing vehicles. Aeroelasticity plays a major role in the design, qualification and certification of flying vehicles, as it contributes to the definition of the flight envelope and affects various performance indicators.
Lecturers: Prof. Carlo Bottaso / Hours: 45 / Semester: 2-3
This module introduces the approaches for the development process of lightweight and aerospace structures, including design, simulation, optimisation and testing aspects. Current structural design concepts for aerospace applications are shown in the context of goals and requirements to be achieved. Possible future developments are addressed and reasons are discussed.
Lecturer: Prof. Horst Baier / Hours: 45 / Semester: 2-3
This module covers various current design methods & relevant design tools for the applied design of surface aircraft. With the simultaneous introduction to the aircraft design system, students are enabled to design both individual components of the aircraft with regard to the overall aircraft, and define the overall aircraft configuration so that it complies with the current requirements with regard to safety, safety and security economy, comfort, the environment and the performance of flights.
Lecturers: Prof. Mirko Hornung / Hours: 45 / Semester: 2-3
This module covers basic phenomenons present in boundary-layers. Physical models and the derivation of the boundary-layer equations from the Navier-Stokes equations are discussed for flat 2-dimensional cases. Temperature, compressible and 3-dimensional boundary-layers are explained. The stability theory explains the laminar-turbulent transition, turbulent boundary-layers and experimental research methods.
Lecturers: Prof. Dr.-ing. Habil. Christian Stemmer / Hours: 45 / Semester: 2-3
This module introduces the main properties & design principles of fibre composite materials and calculation methods. Focusing on Carbon fibre polymers, other types of fibres and matrix materials, failure criteria and behaviour under environmental influences, carbon fibre specific fabrication and manufacturing methods, parameter processing, design and material testing steps will be covered.
Lecturers: Prof Horst Baier / Hours: 45 / Semester: 2-3
This module introduces the basic operating principle of flight controls. Based on the non-linear equations of motion of airplanes and basic control theory principles, control strategies are derived in order to improve the handling qualities or stability of airplanes. In addition, strategies for the implementation of autopilots are presented.
Lecturers: Prof. Florian Holzapfel / Hours: 45 / Semester: 2-3
The content extends over different design requirements and their classification, the sizing process, evaluating the flight performance with respect to power consumption, rotor craft limits and mission design. Additionally, the lecture will cover tools for the cost and weight estimation of the designed rotorcraft.
Lecturers: Prof. Manfred Hajek / Hours: 45 / Semester: 2-3
This module covers Aviation Safety Principles, Basics in Regulations, Airworthiness Code (CS-27, CS-29), Loads, Stress & Fatigue, Performance Categories, Safety Analysis & Flight Accident Investigation. During the presentation of the basic chapters of flight safety and certification the students have the possibility to discuss the important aspects together with the professor. The module covers following chapters such as Aviation Safety Principles, Basics in Regulations Airworthiness Code (CS-27, CS-29), Loads, Stress and Fatigue, Performance Categories, Safety Analysis, and Flight Accident Investigation.
Lecturers: Prof. Manfred Hajek / Hours: 45 / Semester: 2-3
This module addresses the certification process of avionics and flight control systems in commercial aviation. The focus of this lecture lies in safety analysis methods, taking common approaches of their employment in development projects of safety-critical systems in the industry into account. The course begins with giving a general overview of the development and certification of flight control systems, along with the contents of relevant development standards and recommended practices and the resulting process structure. Based on this, profound knowledge of the process and methods of safety assessment of complex technical systems in aircraft is conveyed.
Lecturers: Prof. Florian Holzapfel / Hours: 45 / Semester: 2-3
This module covers astronautical and space engineering topics, and relevant theoretical background and engineering design methods to find suitable solutions for spaceflight and spaceflight technology. The module will be following the processes and technologies from launch (physics of spaceflight, rockets, propulsion, trajectory, spaceflight environment) to orbit with topics in physics (orbital mechanics and dynamics, interplanetary flight, navigation) and engineering subsystem technologies (power, thermal, communication, sensors, actuators). The topics and processes will be presented with practical applications in mind.
Lecturers: Prof. Ulrich Walter and Dr. Martin Rott / Hours: 45 / Semester: 2-3
Choose 1 module from the list below.
The primary purpose of the module is to introduce students to the different areas of business administration, while the final objective is to give them a basic understanding of how to face decision problems in a company. Most importantly, students will analyse long-term investment decisions, how to set up strategic planning in a company, how to gather timely information about the current situation of a company, and how to set up its long-term financial structure.
Lecturers: Prof. Dr. Christoph Kaserer/ Prof. Dr. Isabel Welpe / Hours: 45 / Semester: 1
This module presents the dynamics of technological development through innovation and related management issues, the difference between creating a new product (invention) and improving an existing product/idea (innovation), start-ups and financing of innovation, innovation-driven economic cycles and innovation impact on growth and jobs.
Lecturers: Prof. Dr. Edward Krubasik/ Hours: 45 / Semester: 1
After the completion of coursework, all students have to complete a (minimum) two or three-month internship with the industry or with an academic institution. It is required for the student to complete an internship related to his or her field of study at TUM Asia.
One can secure an internship in Singapore, Germany, or in any other country in Asia, Europe or the rest of the world. Students who have secured a scholarship with their sponsoring company will undergo their internship in the company (this can be conducted in any branch of the company worldwide). Students without an industrial sponsorship are to look for internships independently and it is expected that all students take an active approach about it. TUM Asia will assist to provide students with any possible internship opportunities, but students are to lead the search for internships themselves.
The 6-month long thesis work is the culmination of graduate work and an opportunity to apply the knowledge and skills that students have acquired through course work and research assistant-ships. Through this guided learning experience, students work in collaboration with industry partners or other researchers on a project of mutual interest and may in some cases publish manuscripts resulting from the thesis.
The thesis should be practical-based. Theoretical frameworks or conceptual models may (and should in many cases) guide the research questions. A strictly theoretical paper is not acceptable for a master’s thesis.
Since the timeline for one’s Master studies is quite short, it is important to start exploring and discussing possible thesis topics as early as possible, recommended to be no later than the end of the first term.
After deciding if the thesis project will be carried out in the industry or an university, the student has to find an university supervisor. Professors or the TUM Asia staff will assist the student in finding the right supervisor depending on the programme, but the ownership of the search is still on the student himself or herself. The supervising professor will be a teaching lecturer from the TUM Asia Master programme.
For the completion of the thesis project, the student will have to prepare a written thesis that will be rated by the university supervisor together with (if applicable) the industrial supervisor.
The purpose of the internship is to provide a structured and supervised work experience, in application to the theory work learnt. It is also a platform to develop soft-skills not learnt in the classroom setting and this will help the students to gain job-related skills and achieve their desired career goals.
There will be an informative briefing session conducted for all students to equip them with the necessary knowledge regarding internship and thesis guidelines of TUM Asia. This briefing will be held during the first or second semester of your studies at TUM Asia.
The total tuition fees for this Master programme for the upcoming intake is S$36,000* (before GST).
The tuition fees are to be paid in three instalments as indicated in the table below.
|Registration Fee||1st Instalment||2nd Instalment||3rd Instalment||Total*|
|Deadline for payment||Upon acceptance of offer||1 July||1 December||1 July
(of the next year)
|Gross Amount* (in Singapore dollars, before GST)||S$5,000.00||Split across 3 instalments||S$36,000.00|
|Final Amount* (in Singapore dollars, after GST)||S$5,400.00||Split across 3 instalments||S$38,983.34|
IMPORTANT: The provided information is accurate as of AY2023/24 intake and is subject to change. Students from previous intakes should not refer to the total fee stated on this webpage as their reference.
The respective amounts and payment instructions will be provided in the Student Agreement to all successful applicants.