Ing Ind - Inf (Mag.)(ord. 270) - BV (470) SPACE ENGINEERING - INGEGNERIA SPAZIALE
099266 - PAYLOAD DESIGN
The aim of the course is to provide the competences needed to derive the requirements of a payload instrument for a space mission, starting from given mission objectives and requirements. Given the requirements, the design process is outlined and the reference standards identified.
Risultati di apprendimento attesi
Lectures and exercise sessions will allow students to:
Analyze and understand the scientific objectives and assumptions associated to a space payload instrument
Derive a complete set of design requirements for a space payload instrument
The design laboratory sessions will allow students to:
Write a requirement specification document
Write a mission description document
Perform the preliminary design of a space payload instrument
Summarize and present the results achieved during the design activities
Improve their communication skills
Analysis and definition of requirements: Mission objective definition – preliminary estimation of requirements and mission constraints – design process.
Space Environment: Launch Environment – Near Earth Environment – Deep Space – Planetary environment - Effects on Materials and components.
Testing and Integration: Reference Standard – Structural Testing – Thermal Testing – Electromagnetic compatibility – On-Board Software verification and testing – Mechanical and Electrical Integration – Interface Standard.
Project Management and Control: Project Phases – Schedule control – Documentation – Quality assurance - Introduction to Cost and Risk Analysis.
Students are required to know fundamental concepts of orbital mechanics, structural analysis and thermal analysis as provided by the courses of Obital Mechanics, Spacraft Structures and Heat Transfer and Thermal Analysis.
Modalità di valutazione
Students will be asked to form small groups to which a design project is assigned and partly developed during the design laboratory sessions. Each group will be required to prepare a common report and give a presentation of the design project activity. Finally each students will undergo an individual oral exam on the topic of the classroom lessons.
The report and the group presentation will be required for admission to the individual oral exam. The examinatron is considered successfull if in the individual oral exam the student shows sufficient knowledge and understanding of the topics covered in the lessons.
A.M. Cruise, J.A. Bowles, T.J. Patrick,C.V. Goodall, Principles of Space Instrument Design, Editore: Cambridge University Press
Mohamed M. Abid, Spacecraft Sensors, Editore: John Wiley & Sons
D. Gilmore, Spacecraft Thermal Control Handbook, Vol I: Fundamental Technologies, Editore: AIAA
J.J. Wijker, Spacecraft Structures, Editore: Springer
J. Eickhoff, Onboard Computers, Onboard Software and Satellite Operations, Editore: Springer
M. Eismann, Hyperspectral Remote Sensing, Editore: SPIE Press
W.L. Larson, J.Wertz, Space Mission Analysis and Design, Editore: Kluwer Academic Publishers Group
Tipo Forma Didattica
Ore di attività svolte in aula
Ore di studio autonome
Laboratorio Di Progetto
Informazioni in lingua inglese a supporto dell'internazionalizzazione
Insegnamento erogato in lingua
Disponibilità di materiale didattico/slides in lingua inglese
Disponibilità di libri di testo/bibliografia in lingua inglese
Possibilità di sostenere l'esame in lingua inglese
Disponibilità di supporto didattico in lingua inglese