Mechanical verification logic and first test results for the Euclid spacecraft |
Calvi, Adriano
(European Space Agency/ESTEC)
Bastia, Patrizia (Thales Alenia Space Italy) Suarez, Manuel Perez (Airbus Defence and Space) Neumann, Philipp (SpaceTech GmbH) Carbonell, Albert (RUAG Schweiz AG) |
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 | 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/. |
6 | ECSS-E-ST-32-11C (2008), Space Engineering - Modal Survey Assessment, European Cooperation for Space Standardization, Noordwijk, The Netherlands, https://ecss.nl/. |
7 | ECSS-E-ST-32C Rev.1 (2008), Space Engineering - Structural General Requirements European Cooperation for Space Standardization, Noordwijk, The Netherlands, https://ecss.nl/. |
8 | 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. |
9 | 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. DOI |
10 | Soyuz User's Manual (2012), Issue 2 Rev. 0, Arianespace, https://www.arianespace.com/. |
11 | ECSS-E-HB-32-26A (2013), Spacecraft Mechanical Loads Analysis Handbook, European Cooperation for Space Standardization, Noordwijk, The Netherlands, https://ecss.nl/. |
12 | ECSS-E-ST-10-02C (2009), Space Engineering - Verification, European Cooperation for Space Standardization, Noordwijk, The Netherlands, https://ecss.nl/ |
13 | ECSS-E-ST-10-03C (2012), Space Engineering - Testing, European Cooperation for Space Standardization, Noordwijk, The Netherlands, https://ecss.nl/. |