Advances in aircraft and spacecraft science

  • 제7권3호
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  • Pages.251-269
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  • 2020
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  • 2287-528X(pISSN)
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  • 2287-5271(eISSN)
테크노프레스 (Techno-Press)
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Mechanical verification logic and first test results for the Euclid spacecraft

  • 투고 : 2019.11.22
  • 심사 : 2020.02.11
  • 발행 : 2020.05.25
⟨ 이전 논문 다음 논문 ⟩

초록

Euclid is an optical/near-infrared survey mission of the European Space Agency (ESA) to investigate the nature of dark energy, dark matter and gravity by observing the geometry of the Universe and the formation of structures over cosmological timescales. The Euclid spacecraft mechanical architecture comprises the Payload Module (PLM) and the Service Module (SVM) connected by an interface structure designed to maximize thermal and mechanical decoupling. This paper shortly illustrates the mechanical system of the spacecraft and the mechanical verification philosophy which is based on the Structural and Thermal Model (STM), built at flight standard for structure and thermal qualification and the Proto Flight Model (PFM), used to complete the qualification programme. It will be submitted to a proto-flight test approach and it will be suitable for launch and flight operations. Within the overall verification approach crucial mechanical tests have been successfully performed (2018) on the SVM platform and on the sunshield (SSH) subsystem: the SVM platform static test, the SSH structure modal survey test and the SSH sine vibration qualification test. The paper reports the objectives and the main results of these tests.

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과제정보

The authors are grateful to all colleagues who are involved in the Euclid mechanical systems design, development and verification. All of them, in principle, are contributors to the paper. In particular the authors like to mention: • Marco Cimino and Laura Trittoni, Thales Alenia Space, Italy • Ramon Jimenez Gómez, Airbus Defence and Space, Spain • Dieter Tenhaeff and Tobias Martin, SpaceTech GmbH, Germany • Teresa Pagano, RUAG Schweiz AG • Robert Knockaert, European Space Agency

참고문헌

  1. Bellini, M. and Calvi, A. (2014), "Dynamic analysis and loads definition for the structural design of the Euclid spacecraft", Proceedings of the ISMA 2014 - International Conference on Noise and Vibration Engineering, Leuven, Belgium, September.
  2. Bougoin, M. and Lavenac, J. (2011), "From Herschel to GAIA, 3m-class SiC space optics", Proceedings of the SPIE Optical Engineering + Applications, 2011, San Diego, California, U.S.A., August.
  3. Bougoin, M., Mallet, F., Lavenac, J., Gerbert-Gaillard, A., Ballhause, D. and Chaumeil, F. (2018), "Full-SiC Euclid's very large telescope", Proceedings of the International Conference on Space Optics ICSO 2018, Chania, Greece, October.
  4. Calvi, A. (2016), "Design loads definition and verification strategy for the Euclid spacecraft", Proceedings of the ECSSMET 2016 - European Conference on Spacecraft Structures Materials and Environmental Testing, Toulouse, France, September.
  5. Calvi, A. and Bastia, P. (2016), "Mechanical architecture and loads definition for the design and testing of the Euclid spacecraft", Adv. Aircraft Spacecraft Sci., 3(2) 225-242. http://doi.org/10.12989/aas.2016.3.2.225.
  6. ECSS-E-HB-32-26A (2013), Spacecraft Mechanical Loads Analysis Handbook, European Cooperation for Space Standardization, Noordwijk, The Netherlands, https://ecss.nl/.
  7. ECSS-E-ST-10-02C (2009), Space Engineering - Verification, European Cooperation for Space Standardization, Noordwijk, The Netherlands, https://ecss.nl/
  8. ECSS-E-ST-10-03C (2012), Space Engineering - Testing, European Cooperation for Space Standardization, Noordwijk, The Netherlands, https://ecss.nl/.
  9. ECSS-E-ST-32-10C Rev.1 (2009), Space Engineering - Structural Factors of Safety for Spaceflight Hardware, European Cooperation for Space Standardization, Noordwijk, The Netherlands, https://ecss.nl/.
  10. ECSS-E-ST-32-11C (2008), Space Engineering - Modal Survey Assessment, European Cooperation for Space Standardization, Noordwijk, The Netherlands, https://ecss.nl/.
  11. ECSS-E-ST-32C Rev.1 (2008), Space Engineering - Structural General Requirements European Cooperation for Space Standardization, Noordwijk, The Netherlands, https://ecss.nl/.
  12. Racca, G.D., Laureijs, R., Stagnaro, L., Salvignol, J.C., Alvarez, J.L., Criado, G.S., Venancio, L.G., Short, A., Strada, P., Bonke, T., Colombo, C., Calvi, A., Maiorano, E., Piersanti, O., Prezelus, S., Rosato, P., Pinel, J., Rozemeijer, H., Lesna, V., Musi, P., Sias, M., Anselmi, A., Cazaubiel, V., Vaillon, L., Mellier, Y., Amiaux, J., Berthe, M., Sauvage, M., Azzollini, R., Cropper, M., Pottinger, S., Jahnke, K., Ealet, A., Maciaszek, T., Pasian, F., Zacchei, A., Sacramella, R., Hoar, J., Kohley, R., Vavrek, R., Rudolph, A. and Schmidt, M. (2016), "The Euclid mission design", Proceedings of the Space Telescopes and Instrumentation 2016: Optical, Infrared, and Millimeter Wave, Edinburgh, U.K., June-July.
  13. Soyuz User's Manual (2012), Issue 2 Rev. 0, Arianespace, https://www.arianespace.com/.