Fundamentals of mathematics, physics, and mechanics, as well as basic knowledge of aerospace engineering. Familiarity with programming and basic software tools is recommended but not mandatory.

The course introduces students to the design and engineering of spacecraft, exploring both theoretical foundations and practical applications. It begins with an overview of space vehicles and their subsystems, including structural, thermal, and propulsion systems. Emphasis is placed on understanding the challenges posed by the space environment, such as radiation, microgravity, and thermal extremes.

The second part of the course focuses on systems engineering methodologies, covering the project life cycle, requirements analysis, system architecture, and trade studies. Students will learn to apply techniques such as functional analysis, interface management, and risk assessment to spacecraft design. Additionally, the course addresses cost estimation, technical reviews, and reliability verification.

Special attention is given to modern space architectures, including CubeSats and constellations, as well as mission analysis concepts, enabling students to plan and evaluate space missions effectively. A brief introduction to Mission Analysis is provided, including some case studies where specialized software are used to plan and evaluate space missions.

At the end of the course, the student is expected to be able to:

1. Understand the classification of space vehicles and their subsystems, and identify their roles in space missions;
2. Analyze the challenges posed by the space environment and their impact on spacecraft design and operation;
3. Apply systems engineering principles, including requirements definition, Concept of Operations (ConOps), functional analysis, and trade studies, to spacecraft design;
4. Assess spacecraft costs, risks, and technical performance, and understand the project life cycle phases;

The course is delivered through standard class lectures, where the teacher presents key concepts, methods, and models related to spacecraft architecture and systems engineering. Students are encouraged to actively participate through discussions and questions, fostering a deeper understanding of the topics presented.

Examples and case studies are integrated into the lectures to connect theoretical concepts to real-world applications. Specific attention is given to illustrating the use of systems engineering methodologies through practical examples.

Written or oral exam, depending on student preference

Examination dates are scheduled in accordance with current University regulations. Specific dates will be published on the University website as they are announced

Introduction to space vehicles
The space environment
Spacecraft subsystems
Space Architectures
Constellations
Systems Engineering (SE): Introduction
SE: Project life cycle
SE: System architecture
SE: Scope and ConOps
SE: System hierarchy
SE: Analytical Hierarchy Process
SE: Requirements
SE: Functional analysis, synthesis and design
SE: Interfaces, margins and Technical Performance Measures
SE: Costs and risks
SE: TRL
SE: Trade studies
SE: Reliability and verification
SE: Technical reviews
SE: Schedule and management
Introduction to Mission Analysis

• Fortescue P., Swinerd G., Stark J., Spacecraft Systems Engineering (Fourth Edition), Hoboken, N.J.: John Wiley & Sons, 2011

• NASA, NASA Systems Engineering Handbook (NASA/SP-2016-6105 Rev 2), Washington, D.C.: NASA, 2016

• Wertz J. R., Everett D. F., Puschell J. J. (Eds.) Space Mission Engineering: The New SMAD (vol. 28), Hawthorne, CA: Microcosm Press, 2011