| AERO0018-3 | |||||||||||
| Space experiment development | |||||||||||
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Duration :
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| 30h Th, 30h Pr | |||||||||||
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Number of credits :
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Lecturer :
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| Pierre Rochus | |||||||||||
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Language(s) of instruction :
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| English language | |||||||||||
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Organisation and examination :
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| Teaching in the first semester, review in January | |||||||||||
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Units courses prerequisite and corequisite :
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| Prerequisite or corequisite units are presented within each program | |||||||||||
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Course contents :
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| Spacecraft definition and characteristics
Space environment and constraints Observation and science mission payloads Optical and optoelectronic techniques Mechanical and thermal engineering Detailed contents Space messengers (static fields (gravity, geoids, magnetic field), photons, particles, neutrinos, dust, samples, gravitons and gravitational waves, exoplanets, ...) Why space activities and orbit selection. Information transported by photons. Aerospace and space systems designs compared Reliability and life time On ground environment Launch environment Space environment and impacts on the design of Spacecraft and Instrumentation - Vacuum and its effects - Microgravity and its effects - Temperature cycling and its effects - Outgassing and its effects - Contamination in space - Materials selection - Residual atmosphere - Atomic oxygen - Radiations - Energetic particles, electrons, protons and ions - Induced radiation - Meteorites and orbital debris - Electrical environment (solar wind, magnetosphere, radiation belts, plasma environment) and effects on spacecraft (electrical charging, mission definition, orbit selection, ...) Effects on the optical, mechanical and thermal design Mechanical and dynamical design of instruments Thermal design of instruments Thermal control Scientific missions at ESA and at CSL. Different steps in the design of space instruments - Dimensioning criteria - Integrity-Resistance - Rigidity-Dynamical behavior - Dimensional stability - Specifications for instruments Electromagnetic compatibility (EMC-EMI) Contamination and cleanliness Qualification of instruments |
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Learning outcomes of the course :
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| The courses and practical sessions are presented orally using viewgraphs. The practical work is done in class by students (laptop required to use the software).
Mode of delivery : presence of the students; presentations, Q&A The courses and practical sessions are presented in class. Some practical work can be carried out remotely by the student to better understand the course. |
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Prerequisite knowledge and skills :
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| To acquire more easily the notions of the course, it is recommended (but not required) that the student has the prerequisites
Heat transfer Vibration theory Satellite design Astrodynamics, celestial mechanics For information, the corresponding courses taught at ULg are: "Transfers of heat and matter," Prof. XX "Dynamics of mechanical systems" Prof. J-C. Golinval "Theory of vibrations," Prof. J-C Golinval "Design of satellites," Prof. G. Kerschen "Astrodynamics" Prof. G. Kerschen This course is usually attended by students of two faculties of Science and aplliquées Sciences; the control of acquired knowledge generated by this course will take the past background and future goals of the student into account. |
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Planned learning activities and teaching methods :
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| The courses and practical sessions are presented orally using transparencies. The practical work is done in class by students (laptop required to use the software).
Face-face teaching with Q&A. The courses and practical sessions are presented in class. Some practical work can be carried out remotely by the student to better understand the course. Practical examples are presented and visits can be planned |
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Mode of delivery (face-to-face ; distance-learning) :
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| face to face + Q&A | |||||||||||
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Recommended or required readings :
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| Following books could be useful for additional information :
« Spacecraft Systems Engineering », P.Fortescue, J.Stark, G.Swinerd « Cours de technologie spatiale: Techniques & Technologies des Véhicules Spatiaux » CNES " Handbook of Space Technology" Wilfried Ley/Klaus Wittmann/Willi Hallmann (Editors) « Spacecraft Thermal Control Handbook, Vol I : Fundamental Technologies », D.G Gilmore « Principles of Space Instrument Design », A.M. Cruise, J.A. Bowles, T.J. Patrick, C.V. Goodall « Spacecraft Structures », J.J Wijker « Vibration Analysis for Electronic Equipments », D.S Steinberg « Electronic Imaging in Astronomy ; «Detectors and Instrumentation» Ian s. McLean « Observing Photons in Space » M.C.E. Huber, A. Pauluhn, J.L. Culhane, et al. Eds. « Astronomical Optics » Daniel J. Schroeder « Principles of Optics » Max Born & Emil Wolf « L'observation en Astrophysique » Pierre Léna, Daniel Rouan, |
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Assessment methods and criteria :
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| The final rating of the course is based on: - 30% written exam: exercises and concepts covered in class (with opened book) -70% Oral exam: open questions (from a list of questions - to be confirmed) organizational note The courses are most of the time given at Centre Spatial de Liège to show pratical examples. The course support is written in French / English and the course is taught in French or English depending on the audience. | |||||||||||
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Work placement(s) :
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| Internships and TFE directly related to different aspects of the courses are regularly proposed at CSL | |||||||||||
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Organizational remarks :
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| The course is mostly in Liège Space Centre to allow seeing of live concrete examples.
The course support is written in French / English and the course is taught in French or English following the audience. |
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Contacts :
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| Professor : Pierre ROCHUS, Scientific Director of CSL; prochus@ulg.ac.be 0477372388
Assistant: Lucas Salvador lsalvador@ulg.ac.be +3243824600 ext 663 Library and Intership Management : Florence Defraigne. fdefraigne@ulg.ac.be +3243824600 ext 612 Usually we propose final year projects in such fields as thermal design, mechanical design, optics, electronics, surface engineering...(see http://www.csl.ulg.ac.be/jcms/c_5053/en/home) |
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