Space and astronautical engineering

Educational objectives

The course is focused on the basic elements of the analysis and design of linear control systems.

Educational objectives

The course serves the purpose of giving knowledge of the fundamental properties of compressible flow with
special attention to wave phenomena, their generation, propagation, interaction among themselves and
with bodies, and steepening. Physical description, analytical modeling and numerical solution will be
carefully presented and discussed.

Educational objectives

This course provides the concepts of space flight mechanics and dynamics of structure necessary to perform a preliminary analysis of space missions, defining the requirements of the propulsion system and estimating the consumption of propellant. Are assumed basic knowledge in mechanics courses given in the first degree in Aerospace Engineering, and in particular in Mathematical Methods for Mechanics.

Educational objectives

In addition to the 12 teaching courses provided for by the degree programme of the CdLM AP (degree course), students should seek to attain additional experience. This might be represented by an internship on the premises of a public or private institute, or by participating in design competitions, collaborating in design experiments, taking part in conventions, conferences, seminars or workshops, becoming involved in exhibitions, etc.

Educational objectives

Define the role of space structures within space systems (eg satellites, launchers).
Describe the mechanical environment of space missions.
Provide the fundamental elements for the static and dynamic analysis of space structures.
Describe and analyze the behavior of spatial shell structures and laminated structures in composite material.
Acquire the basic principles of the Finite Element Method, its application and the use of calculation programs based on the method itself.
Introduce the design of space structures in the context of the design of space systems of their development from conception to operational phase up to their disposal to avoid the production of space debris.

Educational objectives

Define the role of space structures within space systems (eg satellites, launchers).
Describe the mechanical environment of space missions.
Provide the fundamental elements for the static and dynamic analysis of space structures.
Describe and analyze the behavior of spatial shell structures and laminated structures in composite material.
Acquire the basic principles of the Finite Element Method, its application and the use of calculation programs based on the method itself.
Introduce the design of space structures in the context of the design of space systems of their development from conception to operational phase up to their disposal to avoid the production of space debris.

Educational objectives

Define the role of space structures within space systems (eg satellites, launchers).
Describe the mechanical environment of space missions.
Provide the fundamental elements for the static and dynamic analysis of space structures.
Describe and analyze the behavior of spatial shell structures and laminated structures in composite material.
Acquire the basic principles of the Finite Element Method, its application and the use of calculation programs based on the method itself.
Introduce the design of space structures in the context of the design of space systems of their development from conception to operational phase up to their disposal to avoid the production of space debris.

Educational objectives

The course provides general knowledge of an electronic
system as a system for information processing. In particular, starting from
basic concepts related to linear systems, the course aims to provide
mathematical tools for signal analysis and basic knowledge of analog and
digital electronics starting from basic components to get to electronics
circuits and finally to more complex electronic systems, focusing on the
application limits due to bandwidth, power and noise for analog and digital
circuits.

Expected learning outcomes: Students will be able to
analyze analog and digital electronic circuits and to design simple electronic
systems.

Educational objectives

Provide basic knowledge on the design of space missions, and on spacecraft navigation and attitude control.
Ability to dimension and design simple systems for orbit and attitude determination and control.
Knowledge of space mission phases and operations.

Educational objectives

The Rocket Propulsion course provides the basic theory and the physical-mathematical tools necessary for the analysis and design of rocket propulsion systems, presents and discusses the main performance parameters of rockets and introduces the main families of chemical rockets by analyzing their characteristic components and their influence on design, performance, cost and environmental impact. The course also provides the student with a series of calculation examples aimed at fixing the theory and comparing it with typical examples of rocket motors used in launchers and in space propulsion.
At the end of the course students must have acquired:
- Knowledge and ability to apply the ideal rocket theory with particular reference to tandem and parallel staging and to the environmental impact generated by propulsive and structural inefficiencies
- Knowledge and ability to apply the theory of steady one-dimensional flows with reference to the typical applications of rocket propelled vehicles
- Knowledge and ability to apply the ideal nozzle theory with particular reference to the main performance parameters and operation in unsuitable conditions
- Knowledge and ability to apply the thermochemistry applied to chemical propulsion with particular reference to relationships with performance parameters and the limits and possibilities of chemical propulsion
- Knowledge of the main combinations of propellants available for chemical propulsion and critical view of the pros and cons of each of them included the toxicity of several combinations and its consequence in terms of production, tests, and costs
- Knowledge of the main components that make up a solid propellant rocket motor and ability to apply the theory of internal zero-dimensional ballistics.
- Knowledge of the main components that make up a liquid propellant rocket engine and ability to estimate its performance according to the propellant properties
- Knowledge of the main development directions of rocket propulsion for applications in the field of launchers and space propulsion with hints to the control of the generation of space debris from launcher upper stages.

Educational objectives

The final test consists in performing a theoretical thesis, experimental design or factual matters relating to the teachings of the Master of Science, to be developed under the guidance of a faculty member of the Council on Learning, in collaboration with public and private, manufacturing and service companies, research centers operating in the area of interest. During the preparation of the thesis, the student must, first, analyze the technical literature on the topic under study. Downstream of this phase, the student will, independently and according to the typology of the thesis:-propose solutions to the problem proposed with a modeling making it possible to analyze the response of the system in correspondence to variations in the characteristic variables of the system;-in the case of experimental work, develop a plan to allow the trial to obtain the desired results. -in the case of project work, dimension, including through the use of computer codes, an aircraft or part of it, highlighting the benefits achieved compared to existing solutions.

Educational objectives

The course is focused on the basic elements of the analysis and design of linear control systems.

Educational objectives

The course serves the purpose of giving knowledge of the fundamental properties of compressible flow with
special attention to wave phenomena, their generation, propagation, interaction among themselves and
with bodies, and steepening. Physical description, analytical modeling and numerical solution will be
carefully presented and discussed.

Educational objectives

This course provides the concepts of space flight mechanics and dynamics of structure necessary to perform a preliminary analysis of space missions, defining the requirements of the propulsion system and estimating the consumption of propellant. Are assumed basic knowledge in mechanics courses given in the first degree in Aerospace Engineering, and in particular in Mathematical Methods for Mechanics.

Educational objectives

In addition to the 12 teaching courses provided for by the degree programme of the CdLM AP (degree course), students should seek to attain additional experience. This might be represented by an internship on the premises of a public or private institute, or by participating in design competitions, collaborating in design experiments, taking part in conventions, conferences, seminars or workshops, becoming involved in exhibitions, etc.

Educational objectives

Define the role of space structures within space systems (eg satellites, launchers).
Describe the mechanical environment of space missions.
Provide the fundamental elements for the static and dynamic analysis of space structures.
Describe and analyze the behavior of spatial shell structures and laminated structures in composite material.
Acquire the basic principles of the Finite Element Method, its application and the use of calculation programs based on the method itself.
Introduce the design of space structures in the context of the design of space systems of their development from conception to operational phase up to their disposal to avoid the production of space debris.

Educational objectives

Define the role of space structures within space systems (eg satellites, launchers).
Describe the mechanical environment of space missions.
Provide the fundamental elements for the static and dynamic analysis of space structures.
Describe and analyze the behavior of spatial shell structures and laminated structures in composite material.
Acquire the basic principles of the Finite Element Method, its application and the use of calculation programs based on the method itself.
Introduce the design of space structures in the context of the design of space systems of their development from conception to operational phase up to their disposal to avoid the production of space debris.

Educational objectives

Define the role of space structures within space systems (eg satellites, launchers).
Describe the mechanical environment of space missions.
Provide the fundamental elements for the static and dynamic analysis of space structures.
Describe and analyze the behavior of spatial shell structures and laminated structures in composite material.
Acquire the basic principles of the Finite Element Method, its application and the use of calculation programs based on the method itself.
Introduce the design of space structures in the context of the design of space systems of their development from conception to operational phase up to their disposal to avoid the production of space debris.

Educational objectives

The course provides general knowledge of an electronic
system as a system for information processing. In particular, starting from
basic concepts related to linear systems, the course aims to provide
mathematical tools for signal analysis and basic knowledge of analog and
digital electronics starting from basic components to get to electronics
circuits and finally to more complex electronic systems, focusing on the
application limits due to bandwidth, power and noise for analog and digital
circuits.

Expected learning outcomes: Students will be able to
analyze analog and digital electronic circuits and to design simple electronic
systems.

Educational objectives

Provide basic knowledge on the design of space missions, and on spacecraft navigation and attitude control.
Ability to dimension and design simple systems for orbit and attitude determination and control.
Knowledge of space mission phases and operations.

Educational objectives

The Rocket Propulsion course provides the basic theory and the physical-mathematical tools necessary for the analysis and design of rocket propulsion systems, presents and discusses the main performance parameters of rockets and introduces the main families of chemical rockets by analyzing their characteristic components and their influence on design, performance, cost and environmental impact. The course also provides the student with a series of calculation examples aimed at fixing the theory and comparing it with typical examples of rocket motors used in launchers and in space propulsion.
At the end of the course students must have acquired:
- Knowledge and ability to apply the ideal rocket theory with particular reference to tandem and parallel staging and to the environmental impact generated by propulsive and structural inefficiencies
- Knowledge and ability to apply the theory of steady one-dimensional flows with reference to the typical applications of rocket propelled vehicles
- Knowledge and ability to apply the ideal nozzle theory with particular reference to the main performance parameters and operation in unsuitable conditions
- Knowledge and ability to apply the thermochemistry applied to chemical propulsion with particular reference to relationships with performance parameters and the limits and possibilities of chemical propulsion
- Knowledge of the main combinations of propellants available for chemical propulsion and critical view of the pros and cons of each of them included the toxicity of several combinations and its consequence in terms of production, tests, and costs
- Knowledge of the main components that make up a solid propellant rocket motor and ability to apply the theory of internal zero-dimensional ballistics.
- Knowledge of the main components that make up a liquid propellant rocket engine and ability to estimate its performance according to the propellant properties
- Knowledge of the main development directions of rocket propulsion for applications in the field of launchers and space propulsion with hints to the control of the generation of space debris from launcher upper stages.

Educational objectives

The final test consists in performing a theoretical thesis, experimental design or factual matters relating to the teachings of the Master of Science, to be developed under the guidance of a faculty member of the Council on Learning, in collaboration with public and private, manufacturing and service companies, research centers operating in the area of interest. During the preparation of the thesis, the student must, first, analyze the technical literature on the topic under study. Downstream of this phase, the student will, independently and according to the typology of the thesis:-propose solutions to the problem proposed with a modeling making it possible to analyze the response of the system in correspondence to variations in the characteristic variables of the system;-in the case of experimental work, develop a plan to allow the trial to obtain the desired results. -in the case of project work, dimension, including through the use of computer codes, an aircraft or part of it, highlighting the benefits achieved compared to existing solutions.

Educational objectives

The course is focused on the basic elements of the analysis and design of linear control systems.

Educational objectives

The course serves the purpose of giving knowledge of the fundamental properties of compressible flow with
special attention to wave phenomena, their generation, propagation, interaction among themselves and
with bodies, and steepening. Physical description, analytical modeling and numerical solution will be
carefully presented and discussed.

Educational objectives

This course provides the concepts of space flight mechanics and dynamics of structure necessary to perform a preliminary analysis of space missions, defining the requirements of the propulsion system and estimating the consumption of propellant. Are assumed basic knowledge in mechanics courses given in the first degree in Aerospace Engineering, and in particular in Mathematical Methods for Mechanics.

Educational objectives

In addition to the 12 teaching courses provided for by the degree programme of the CdLM AP (degree course), students should seek to attain additional experience. This might be represented by an internship on the premises of a public or private institute, or by participating in design competitions, collaborating in design experiments, taking part in conventions, conferences, seminars or workshops, becoming involved in exhibitions, etc.

Educational objectives

Define the role of space structures within space systems (eg satellites, launchers).
Describe the mechanical environment of space missions.
Provide the fundamental elements for the static and dynamic analysis of space structures.
Describe and analyze the behavior of spatial shell structures and laminated structures in composite material.
Acquire the basic principles of the Finite Element Method, its application and the use of calculation programs based on the method itself.
Introduce the design of space structures in the context of the design of space systems of their development from conception to operational phase up to their disposal to avoid the production of space debris.

Educational objectives

Define the role of space structures within space systems (eg satellites, launchers).
Describe the mechanical environment of space missions.
Provide the fundamental elements for the static and dynamic analysis of space structures.
Describe and analyze the behavior of spatial shell structures and laminated structures in composite material.
Acquire the basic principles of the Finite Element Method, its application and the use of calculation programs based on the method itself.
Introduce the design of space structures in the context of the design of space systems of their development from conception to operational phase up to their disposal to avoid the production of space debris.

Educational objectives

Define the role of space structures within space systems (eg satellites, launchers).
Describe the mechanical environment of space missions.
Provide the fundamental elements for the static and dynamic analysis of space structures.
Describe and analyze the behavior of spatial shell structures and laminated structures in composite material.
Acquire the basic principles of the Finite Element Method, its application and the use of calculation programs based on the method itself.
Introduce the design of space structures in the context of the design of space systems of their development from conception to operational phase up to their disposal to avoid the production of space debris.

Educational objectives

The course provides general knowledge of an electronic
system as a system for information processing. In particular, starting from
basic concepts related to linear systems, the course aims to provide
mathematical tools for signal analysis and basic knowledge of analog and
digital electronics starting from basic components to get to electronics
circuits and finally to more complex electronic systems, focusing on the
application limits due to bandwidth, power and noise for analog and digital
circuits.

Expected learning outcomes: Students will be able to
analyze analog and digital electronic circuits and to design simple electronic
systems.

Educational objectives

Provide basic knowledge on the design of space missions, and on spacecraft navigation and attitude control.
Ability to dimension and design simple systems for orbit and attitude determination and control.
Knowledge of space mission phases and operations.

Educational objectives

The Rocket Propulsion course provides the basic theory and the physical-mathematical tools necessary for the analysis and design of rocket propulsion systems, presents and discusses the main performance parameters of rockets and introduces the main families of chemical rockets by analyzing their characteristic components and their influence on design, performance, cost and environmental impact. The course also provides the student with a series of calculation examples aimed at fixing the theory and comparing it with typical examples of rocket motors used in launchers and in space propulsion.
At the end of the course students must have acquired:
- Knowledge and ability to apply the ideal rocket theory with particular reference to tandem and parallel staging and to the environmental impact generated by propulsive and structural inefficiencies
- Knowledge and ability to apply the theory of steady one-dimensional flows with reference to the typical applications of rocket propelled vehicles
- Knowledge and ability to apply the ideal nozzle theory with particular reference to the main performance parameters and operation in unsuitable conditions
- Knowledge and ability to apply the thermochemistry applied to chemical propulsion with particular reference to relationships with performance parameters and the limits and possibilities of chemical propulsion
- Knowledge of the main combinations of propellants available for chemical propulsion and critical view of the pros and cons of each of them included the toxicity of several combinations and its consequence in terms of production, tests, and costs
- Knowledge of the main components that make up a solid propellant rocket motor and ability to apply the theory of internal zero-dimensional ballistics.
- Knowledge of the main components that make up a liquid propellant rocket engine and ability to estimate its performance according to the propellant properties
- Knowledge of the main development directions of rocket propulsion for applications in the field of launchers and space propulsion with hints to the control of the generation of space debris from launcher upper stages.

Educational objectives

The final test consists in performing a theoretical thesis, experimental design or factual matters relating to the teachings of the Master of Science, to be developed under the guidance of a faculty member of the Council on Learning, in collaboration with public and private, manufacturing and service companies, research centers operating in the area of interest. During the preparation of the thesis, the student must, first, analyze the technical literature on the topic under study. Downstream of this phase, the student will, independently and according to the typology of the thesis:-propose solutions to the problem proposed with a modeling making it possible to analyze the response of the system in correspondence to variations in the characteristic variables of the system;-in the case of experimental work, develop a plan to allow the trial to obtain the desired results. -in the case of project work, dimension, including through the use of computer codes, an aircraft or part of it, highlighting the benefits achieved compared to existing solutions.

Educational objectives

The course is focused on the basic elements of the analysis and design of linear control systems.

Educational objectives

The course aims at providing
the conceptual and analytical skills needed to understand the structure of
radio systems and sensors, with specific reference to telecommunications,
radiolocation and radar applications:

a) the structure of a radio
transceiver, by specifically identifying the main elements needed for its
preliminary design;

b) the impact of the
simplified signal propagation models for the satellite transmissions on the
power budget and time delays;

c) understanding the global
functional scheme of satellite radio location systems and their performance
evaluation;

d) understanding the specific characteristics
of the radar systems for surveillance and imaging, as well as the satellite
radiocommunication systems.

Educational objectives

The course aims at providing
the conceptual and analytical skills needed to understand the structure of
radio systems and sensors, with specific reference to telecommunications,
radiolocation and radar applications:

a) the structure of a radio
transceiver, by specifically identifying the main elements needed for its
preliminary design;

b) the impact of the
simplified signal propagation models for the satellite transmissions on the
power budget and time delays;

c) understanding the global
functional scheme of satellite radio location systems and their performance
evaluation;

d) understanding the specific characteristics
of the radar systems for surveillance and imaging, as well as the satellite
radiocommunication systems.

Educational objectives

The course aims at providing
the conceptual and analytical skills needed to understand the structure of
radio systems and sensors, with specific reference to telecommunications,
radiolocation and radar applications:

a) the structure of a radio
transceiver, by specifically identifying the main elements needed for its
preliminary design;

b) the impact of the
simplified signal propagation models for the satellite transmissions on the
power budget and time delays;

c) understanding the global
functional scheme of satellite radio location systems and their performance
evaluation;

d) understanding the specific characteristics
of the radar systems for surveillance and imaging, as well as the satellite
radiocommunication systems.

Educational objectives

The module describes the techniques for quantitative remote sensing in the microwave spectrum with both passive (microwave radiometers) and active (radar) sensors and their role in the development of the European Union Copernicus services for monitoring our planet and its environment with the help of satellite data. It illustrates the main applications and methods for the extraction of geophysical parameters of the atmosphere, the sea and emerged surfaces (soil and vegetation). Among these, microwave sensors support in particular the monitoring of the hydrological cycle and that of both agricultural and forest vegetation and the control of disastrous phenomena (floods, earthquakes, droughts) in a context of sustainable use of earth resources, monitoring of changes climate and protection of the natural environment.
The module provides the physical bases and models for the quantitative interpretation of remote sensing data, and in particular the electromagnetic models for the analysis of emission, absorption and diffusion problems by natural means (atmosphere, rough sea surface, soil and vegetated layers).

Educational objectives

This course provides the concepts of space flight mechanics and dynamics of structure necessary to perform a preliminary analysis of space missions, defining the requirements of the propulsion system and estimating the consumption of propellant. Are assumed basic knowledge in mechanics courses given in the first degree in Aerospace Engineering, and in particular in Mathematical Methods for Mechanics.

Educational objectives

In addition to the 12 teaching courses provided for by the degree programme of the CdLM AP (degree course), students should seek to attain additional experience. This might be represented by an internship on the premises of a public or private institute, or by participating in design competitions, collaborating in design experiments, taking part in conventions, conferences, seminars or workshops, becoming involved in exhibitions, etc.

Educational objectives

Define the role of space structures within space systems (eg satellites, launchers).
Describe the mechanical environment of space missions.
Provide the fundamental elements for the static and dynamic analysis of space structures.
Describe and analyze the behavior of spatial shell structures and laminated structures in composite material.
Acquire the basic principles of the Finite Element Method, its application and the use of calculation programs based on the method itself.
Introduce the design of space structures in the context of the design of space systems of their development from conception to operational phase up to their disposal to avoid the production of space debris.

Educational objectives

Define the role of space structures within space systems (eg satellites, launchers).
Describe the mechanical environment of space missions.
Provide the fundamental elements for the static and dynamic analysis of space structures.
Describe and analyze the behavior of spatial shell structures and laminated structures in composite material.
Acquire the basic principles of the Finite Element Method, its application and the use of calculation programs based on the method itself.
Introduce the design of space structures in the context of the design of space systems of their development from conception to operational phase up to their disposal to avoid the production of space debris.

Educational objectives

Define the role of space structures within space systems (eg satellites, launchers).
Describe the mechanical environment of space missions.
Provide the fundamental elements for the static and dynamic analysis of space structures.
Describe and analyze the behavior of spatial shell structures and laminated structures in composite material.
Acquire the basic principles of the Finite Element Method, its application and the use of calculation programs based on the method itself.
Introduce the design of space structures in the context of the design of space systems of their development from conception to operational phase up to their disposal to avoid the production of space debris.

Educational objectives

Electronics module (6 credits)
The electronics module intends to provide the general knowledge of an electronic system intended as an information processing system. In particular, starting from the basic concepts related to linear systems, the course aims to provide the mathematical tools for the analysis of signals and the basic knowledge of analog and digital electronics starting from the fundamental components to get to electronic circuits and finally to systems more complex electronics. The course focuses on the link between frequency band, power consumption and noise in analog circuits and digital networks for space and satellite applications in the context of transport, energy and telecommunications infrastructures.
Expected learning outcomes: students will be able to analyze analog and digital electronic circuits and will acquire design elements of electronic systems for different application fields.
Optical sensor module (3 credits)
The optical sensor module aims to provide an introduction to integrated optical systems starting from the mechanisms of transduction of radiation through optical sources (lasers and LEDs) and semiconductor photodetectors up to understanding the system-level aspects of sensors of CCD and CMOS based images. The module presents application cases in the field of environmental remote sensing and broadband optical communications in fiber and in free space and for complex systems.
Expected learning outcomes: students will be able to understand the functioning of image and environmental sensors, comparing the performance of the different technologies available according to the system requirements.

Educational objectives

Electronics module (6 credits)
The electronics module intends to provide the general knowledge of an electronic system intended as an information processing system. In particular, starting from the basic concepts related to linear systems, the course aims to provide the mathematical tools for the analysis of signals and the basic knowledge of analog and digital electronics starting from the fundamental components to get to electronic circuits and finally to systems more complex electronics. The course focuses on the link between frequency band, power consumption and noise in analog circuits and digital networks for space and satellite applications in the context of transport, energy and telecommunications infrastructures.
Expected learning outcomes: students will be able to analyze analog and digital electronic circuits and will acquire design elements of electronic systems for different application fields.
Optical sensor module (3 credits)
The optical sensor module aims to provide an introduction to integrated optical systems starting from the mechanisms of transduction of radiation through optical sources (lasers and LEDs) and semiconductor photodetectors up to understanding the system-level aspects of sensors of CCD and CMOS based images. The module presents application cases in the field of environmental remote sensing and broadband optical communications in fiber and in free space and for complex systems.
Expected learning outcomes: students will be able to understand the functioning of image and environmental sensors, comparing the performance of the different technologies available according to the system requirements.

Educational objectives

Electronics module (6 credits)
The electronics module intends to provide the general knowledge of an electronic system intended as an information processing system. In particular, starting from the basic concepts related to linear systems, the course aims to provide the mathematical tools for the analysis of signals and the basic knowledge of analog and digital electronics starting from the fundamental components to get to electronic circuits and finally to systems more complex electronics. The course focuses on the link between frequency band, power consumption and noise in analog circuits and digital networks for space and satellite applications in the context of transport, energy and telecommunications infrastructures.
Expected learning outcomes: students will be able to analyze analog and digital electronic circuits and will acquire design elements of electronic systems for different application fields.
Optical sensor module (3 credits)
The optical sensor module aims to provide an introduction to integrated optical systems starting from the mechanisms of transduction of radiation through optical sources (lasers and LEDs) and semiconductor photodetectors up to understanding the system-level aspects of sensors of CCD and CMOS based images. The module presents application cases in the field of environmental remote sensing and broadband optical communications in fiber and in free space and for complex systems.
Expected learning outcomes: students will be able to understand the functioning of image and environmental sensors, comparing the performance of the different technologies available according to the system requirements.

Educational objectives

Provide basic knowledge on the design of space missions, and on spacecraft navigation and attitude control.
Ability to dimension and design simple systems for orbit and attitude determination and control.
Knowledge of space mission phases and operations.

Educational objectives

Provide a fundamental knowledge of in-space propulsion systems, i.e., thrusters which are used in space missions for a variety of applications, including deep space exploration, attitude control and station keeping. Provide the necessary tools and models for analyzing the operation and performance of electrothermal, electrostatic, electromagnetic, and nuclear thermal rockets. Attention will be devoted to "green" alternatives to conventional chemical propulsion systems for future spacecraft to improve overall propellant efficiency, while reducing the handling concerns associated with the usage of toxic fuels.

Educational objectives

Fluid mechanics of the Earth and planets, including oceans, atmospheres and interiors, and the fluid mechanics of the sun. In addition, their magneto-hydrodynamic behaviors are investigated.

Educational objectives

The final test consists in performing a theoretical thesis, experimental design or factual matters relating to the teachings of the Master of Science, to be developed under the guidance of a faculty member of the Council on Learning, in collaboration with public and private, manufacturing and service companies, research centers operating in the area of interest. During the preparation of the thesis, the student must, first, analyze the technical literature on the topic under study. Downstream of this phase, the student will, independently and according to the typology of the thesis:-propose solutions to the problem proposed with a modeling making it possible to analyze the response of the system in correspondence to variations in the characteristic variables of the system;-in the case of experimental work, develop a plan to allow the trial to obtain the desired results. -in the case of project work, dimension, including through the use of computer codes, an aircraft or part of it, highlighting the benefits achieved compared to existing solutions.

Educational objectives

The course is focused on the basic elements of the analysis and design of linear control systems.

Educational objectives

The course aims at developing the fundamental engineering aspects of orbital and attitude dynamics of rigid spacecraft, starting from ideal conditions (Keplerian motion and free-spinning spacecraft), then including relevant practical aspects, such as the effects of perturbing and control force and torques, up to the determination of control and maneuver strategies in response of mission requirements. At the end of the course, the student is expected 1) to understand the most relevant aspects of spacecraft dynamic behavior; 2) to solve problems which requires the determination of orbit features, orbital maneuvers or characterize attitude motion of a rigid spacecraft.

Educational objectives

The main objective of the course is to introduce the student to fundamental laws governing compressible flows, under subsonic and supersonic conditions. During a first phase the solution of quasi-1D flows will be approached, with application to nozzle, air intake and supersonic wind tunnels. In the following application to subsonic and supersonic wing will be conducted. Basic knowledge of hypersonic flows: Newtonian theory.
Numerical tools for simulation of compressible flows will be provided. The main objective is to introduce the student to the modern techniques of numerical analysis applied to gas dynamics. The main focus will be on the definition of general criteria for the development of numerical schemes and on their implementation in numerical codes for the solution of the multi-dimensional Euler equations.

Educational objectives

The main objective of the course is to introduce the student to fundamental laws governing compressible flows, under subsonic and supersonic conditions. During a first phase the solution of quasi-1D flows will be approached, with application to nozzle, air intake and supersonic wind tunnels. In the following application to subsonic and supersonic wing will be conducted. Basic knowledge of hypersonic flows: Newtonian theory.
Numerical tools for simulation of compressible flows will be provided. The main objective is to introduce the student to the modern techniques of numerical analysis applied to gas dynamics. The main focus will be on the definition of general criteria for the development of numerical schemes and on their implementation in numerical codes for the solution of the multi-dimensional Euler equations.

Educational objectives

The main objective of the course is to introduce the student to fundamental laws governing compressible flows, under subsonic and supersonic conditions. During a first phase the solution of quasi-1D flows will be approached, with application to nozzle, air intake and supersonic wind tunnels. In the following application to subsonic and supersonic wing will be conducted. Basic knowledge of hypersonic flows: Newtonian theory.
Numerical tools for simulation of compressible flows will be provided. The main objective is to introduce the student to the modern techniques of numerical analysis applied to gas dynamics. The main focus will be on the definition of general criteria for the development of numerical schemes and on their implementation in numerical codes for the solution of the multi-dimensional Euler equations.

Educational objectives

In addition to the 12 teaching courses provided for by the degree programme of the CdLM AP (degree course), students should seek to attain additional experience. This might be represented by an internship on the premises of a public or private institute, or by participating in design competitions, collaborating in design experiments, taking part in conventions, conferences, seminars or workshops, becoming involved in exhibitions, etc.

Educational objectives

Provide students with the methodologies for the evaluation of mechanical stresses and analyzes necessary for the study and design of structures in the aerospace field (eg wings, launchers, satellites). Introduction to structural design criteria based on the sustainability of the production cycle and global energy efficiency. Analytical methods for the study of thin-walled structures and aeronautical shells will be studied in depth, both in the static and dynamic fields. To provide the fundamental knowledge for the study of structural behavior through the Finite Element Method.

Educational objectives

Provide students with the methodologies for the evaluation of mechanical stresses and analyzes necessary for the study and design of structures in the aerospace field (eg wings, launchers, satellites). Introduction to structural design criteria based on the sustainability of the production cycle and global energy efficiency. Analytical methods for the study of thin-walled structures and aeronautical shells will be studied in depth, both in the static and dynamic fields. To provide the fundamental knowledge for the study of structural behavior through the Finite Element Method.

Educational objectives

Provide students with the methodologies for the evaluation of mechanical stresses and analyzes necessary for the study and design of structures in the aerospace field (eg wings, launchers, satellites). Introduction to structural design criteria based on the sustainability of the production cycle and global energy efficiency. Analytical methods for the study of thin-walled structures and aeronautical shells will be studied in depth, both in the static and dynamic fields. To provide the fundamental knowledge for the study of structural behavior through the Finite Element Method.

Educational objectives

Provide basic knowledge on the design of space missions, and on spacecraft navigation and attitude control.
Ability to dimension and design simple systems for orbit and attitude determination and control.
Knowledge of space mission phases and operations.

Educational objectives

The Rocket Propulsion course provides the basic theory and the physical-mathematical tools necessary for the analysis and design of rocket propulsion systems, presents and discusses the main performance parameters of rockets and introduces the main families of chemical rockets by analyzing their characteristic components and their influence on design, performance, cost and environmental impact. The course also provides the student with a series of calculation examples aimed at fixing the theory and comparing it with typical examples of rocket motors used in launchers and in space propulsion.
At the end of the course students must have acquired:
- Knowledge and ability to apply the ideal rocket theory with particular reference to tandem and parallel staging and to the environmental impact generated by propulsive and structural inefficiencies
- Knowledge and ability to apply the theory of steady one-dimensional flows with reference to the typical applications of rocket propelled vehicles
- Knowledge and ability to apply the ideal nozzle theory with particular reference to the main performance parameters and operation in unsuitable conditions
- Knowledge and ability to apply the thermochemistry applied to chemical propulsion with particular reference to relationships with performance parameters and the limits and possibilities of chemical propulsion
- Knowledge of the main combinations of propellants available for chemical propulsion and critical view of the pros and cons of each of them included the toxicity of several combinations and its consequence in terms of production, tests, and costs
- Knowledge of the main components that make up a solid propellant rocket motor and ability to apply the theory of internal zero-dimensional ballistics.
- Knowledge of the main components that make up a liquid propellant rocket engine and ability to estimate its performance according to the propellant properties
- Knowledge of the main development directions of rocket propulsion for applications in the field of launchers and space propulsion with hints to the control of the generation of space debris from launcher upper stages.

Educational objectives

The final test consists in performing a theoretical thesis, experimental design or factual matters relating to the teachings of the Master of Science, to be developed under the guidance of a faculty member of the Council on Learning, in collaboration with public and private, manufacturing and service companies, research centers operating in the area of interest. During the preparation of the thesis, the student must, first, analyze the technical literature on the topic under study. Downstream of this phase, the student will, independently and according to the typology of the thesis:-propose solutions to the problem proposed with a modeling making it possible to analyze the response of the system in correspondence to variations in the characteristic variables of the system;-in the case of experimental work, develop a plan to allow the trial to obtain the desired results. -in the case of project work, dimension, including through the use of computer codes, an aircraft or part of it, highlighting the benefits achieved compared to existing solutions.