Validation of the Structural-Thermal-Model of the Small Earth Observation Satellite Flying Laptop; ; et al Poster (2013, April 10) Thorough thermal design and testing is compulsory for every satellite mission. A well-known thermal behavior of the entire satellite system is therefore indispensable and needs to be verified during the ... [more ▼] Thorough thermal design and testing is compulsory for every satellite mission. A well-known thermal behavior of the entire satellite system is therefore indispensable and needs to be verified during the spacecraft development. A Structural-Thermal-Model (STM) was constructed for the Flying Laptop, a satellite currently being developed at the Institute of Space Systems (IRS) of the University of Stuttgart, which enables the validation of mechanical and thermal simulations for the satellite’s Flight-Model. The STM was vibration and thermal-vacuum tested at the Centre Spatial Liège (CSL). This paper will de-scribe the design and construction of the STM as well as the facilities and test equipment used for the tests. Conclusions will be drawn from the actual test results. [less ▲] Detailed reference viewed: 13 (5 ULg) Validation of the Structural-Thermal Model of the Small Earth Observation Satellite Flying Laptop; ; et al in Selected Proceedings of the 9th IAA International Symposium on Small Satellites for Earth Observation (2013, April 10) Thorough thermal design and testing is compulsory for every satellite mission. A well-known thermal behavior of the entire satellite system is therefore indispensable and needs to be verified during the ... [more ▼] Thorough thermal design and testing is compulsory for every satellite mission. A well-known thermal behavior of the entire satellite system is therefore indispensable and needs to be verified during the spacecraft development. A Structural-Thermal-Model (STM) was constructed for the Flying Laptop, a satellite currently being developed at the Institute of Space Systems (IRS) of the University of Stuttgart, which enables the validation of mechanical and thermal simulations for the satellite’s Flight-Model. The STM was vibration and thermal-vacuum tested at the Centre Spatial Liège (CSL). This paper will de-scribe the design and construction of the STM as well as the facilities and test equipment used for the tests. Conclusions will be drawn from the actual test results. [less ▲] Detailed reference viewed: 20 (16 ULg) Small satellite activities at the University of LiègeSalvador, Lucas ; Rochus, Pierre ![]() Poster (2012, October 01) Detailed reference viewed: 26 (12 ULg) The Uranus System Explorer (USE) – Unveiling the evolution and formation of icy giants; ; et al Conference (2012, September) The results presented are the output of a student exercise carried out at the Alpbach Summer School 2012 , the topic of which pertained to the exploration of the giant planets and their systems. In this ... [more ▼] The results presented are the output of a student exercise carried out at the Alpbach Summer School 2012 , the topic of which pertained to the exploration of the giant planets and their systems. In this context, we propose in this paper the Uranus System Explorer (USE), a mission to investigate the Uranus planetary system and gain new insight into the formation and evolution of icy giants. [less ▲] Detailed reference viewed: 47 (14 ULg) The Uranus System Explorer (USE) – Unveiling the evolution and formation of icy giants; ; et al Poster (2012, September) Detailed reference viewed: 20 (6 ULg) |
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