Liébecq, S. (2023). EUCLID Payload Module : Thermal Balance and Thermal Vacuum Test at CSL Premises. In European Conference on Spacecraft Structures Materials and Environmental Testing. Toulouse, France: CNES. |
Rochus, P., Auchère, F., Berghmans, D., Harra, L., Schmutz, W., Schühle, U., Addison, P., Appourchaux, T., Aznar Cuadrado, R., Baker, D., Barbay, J., Bates, D., Benmoussa, A., Bergmann, M., Beurthe, C., Borgo, B., Bonte, K., Bouzit, M., Bradley, L., ... Zhukov, A. N. (September 2022). Erratum: The Solar Orbiter EUI instrument: The Extreme Ultraviolet Imager (A&A, (2020) 642 A8 DOI: 10.1051/0004-6361/201936663). Astronomy and Astrophysics, 665, 1. doi:10.1051/0004-6361/201936663e |
Rochus, P., Auchère, F., Berghmans, D., Harra, L., Schmutz, W., Schühle, U., Addison, P., Appourchaux, T., Aznar Cuadrado, R., Baker, D., Barbay, J., Bates, D., BenMoussa, A., Bergmann, M., Beurthe, C., Borgo, B., Bonte, K., Bouzit, M., Bradley, L., ... Zhukov, A. N. (01 October 2020). The Solar Orbiter EUI instrument: The Extreme Ultraviolet Imager. Astronomy and Astrophysics, 642, 8. doi:10.1051/0004-6361/201936663 |
Carapelle, A., Grodent, D., Langevin, Y., Carter, J., Arondel, A., Vincendon, M., Guiot, P., Retherford, K., Davis, M., Liébecq, S., & Renotte, E. (01 February 2019). New low electron flux facility in the 0 to 3.5 MeV range for the study of induced signal in JUICE instruments: UVS and MAJIS measurements. Nuclear Instruments and Methods in Physics Research. Section B, Beam Interactions with Materials and Atoms, 440, 197-200. doi:10.1016/j.nimb.2018.04.029 |
Grodent, C., Domken, I., Tychon, I., Liébecq, S., Samain, V., wimmer, R., davidson, M., barthes, J.-C., lecrenier, O., & elfving, A. (October 2018). The aeolus spacecraft TVAC full qualification at Centre Spatial de Liège premises, description and challenges [Paper presentation]. 31st Aerospace Testing Seminar, Los Angeles, USA. |
Grodent, C., Thibert, T., Marquet, B., Liébecq, S., Lebranchu, C., Bongers, E., Ifrim, D., Stanica, C., Popa, I., Cancescu, A., & Schnorhk, A. (October 2018). Wide Range Temperature Thermal Test Facility for JUICE large appendages [Paper presentation]. 31st Aerospace Testing Seminar, Los Angeles, USA. |
Grodent, C., Domken, I., Tychon, I., Liébecq, S., Samain, V., wimmer, R., Davidson, M., Barthes, J.-C., Lecrenier, O., & Elfving, A. (May 2018). The Aeolus Spacecraft TVAC full qualification at Centre Spatial de Liège premises, description and challenges [Paper presentation]. ECSSMET 2018, Noordwijk, The Netherlands. |
Grodent, C., Thibert, T., Marquet, B., Liébecq, S., Tychon, I., Guiot, M., jamotton, P., lebranchu, C., bongers, E., ifrim, D., stanica, C., popa, I., cancescu, A., & schnorhk, A. (2018). Wide Range Thermal Test Facility for JUICE large appendages, Design and Results. In Proceedings of the European Conference on Spacecraft Structures, Materials and Environmental Testing - ECSSMET 2018. Noordwijk, Netherlands: ESA. |
Carapelle, A., Grodent, D., Langevin, Y., Carter, J., Arondel, A., Vincendon, M., Guiot, P., Retherford, K., Davis, M., Liébecq, S., & Renotte, E. (October 2017). New low electron flux facility in the 0 to 3.5 MeV range for the study of induced signal in JUICE instruments: UVS and MAJIS measurements [Poster presentation]. RADECS 2017, Genève, Switzerland. |
Grodent, C., Thibert, T., Liébecq, S., jamotton, P., salvador, L., lebranchu, C., schirmann, T., schnorhk, A., ifrim, D., & stanica, C. (November 2016). Wide Range Thermal Test Facility for JUICE large appendages [Paper presentation]. 29th Space Simulation Conference, Annapolis, USA. |
Grodent, C., Thibert, T., Liébecq, S., jamotton, P., salvador, L., lebranchu, C., schirmann, T., schnorhk, A., ifrim, D., & stanica, C. (September 2016). Wide Range Thermal Test Facility for JUICE large appendages [Paper presentation]. 14th European Conference on Spacecraft Structures, Materials and Environmental Testing, Toulouse, France. |
Renotte, E., Denis, F., Desselle, R., Fleury-Frenette, K., Galy, C., Gillis, J.-M., Graas, E., Liébecq, S., Salvador, L., Servaye, J.-S., Stockman, Y., & Thizy, C. (2016). Recent achievements on ASPIICS, an externally occulted coronagraph for PROBA-3. Proceedings of SPIE: The International Society for Optical Engineering. doi:10.1117/12.2232695 |
Grodent, C., Liébecq, S., Hellin, M.-L., Blain, P., Languy, F., Samain, V., Marcotte, S., Brevers, S., Domken, I., Tychon, I., dingjan, J., merlin, C., ninane, N., & jamotton, P. (October 2015). TROPOMI instrument (ESA Sentinel 5-P): environmental tests at CSL [Paper presentation]. 29th Aerospace Testing Seminar. |
Renotte, E., Alia, A., Bemporad, A., Bernier, J., Bramanti, C., Bucklet, S., Capobianco, G., Cernica, I., Daniel, V., Darakchiev, R., Darmetko, M., Debaize, A., Denis, F., Desselle, R., De Vos, L., Dinescu, A., Fineschi, S., Fleury-Frenette, K., Focardi, M., ... Zhukov, A. (2015). Design status of ASPIICS, an externally occulted coronagraph for PROBA-3. In Proc. SPIE Volume 9604 Solar Physics and Space Weather Instrumentation VI. doi:10.1117/12.2186962 |
Jacques, L., Halain, J.-P., Rossi, L., Hellin, M.-L., Jamotton, P., Liébecq, S., Mazzoli, A., Renotte, E., & Rochus, P. (26 March 2015). Thermal Balance Test of Solar Orbiter EUI Instrument Structural and Thermal Model with 13 Solar Constants [Paper presentation]. Spacecraft Thermal Control Workshop, El Segundo, United States. |
Rossi, L., zhukova, M., Jacques, L., Halain, J.-P., Hellin, M.-L., Jamotton, P., Renotte, E., Rochus, P., Liébecq, S., & Mazzoli, A. (2014). Solar simulation test up to 13 solar constants for the thermal balance of the Solar Orbiter EUI instrument. Proceedings of SPIE: The International Society for Optical Engineering. doi:10.1117/12.2055125 |
Jamotton, P., Liébecq, S., & Samain, V. (2013). Optical Samples Quick Automatic Cryogenic Cycling at CSL. In Cryo Workshop. |
Domken, I., Plesseria, J.-Y., Mazy, E. (Other coll.), Rossi, L. (Other coll.), Hellin, M.-L. (Other coll.), Marcotte, S. (Other coll.), Liébecq, S. (Other coll.), Tychon, I. (Other coll.), Renotte, E. (Other coll.), Grodent, C. (Other coll.), Thome, M. (Other coll.), & Cucchiaro, A. (Other coll.). (2011). 26th Aerospace Testing Seminar at Los Angeles (March 29-31, 2011) MSI Instrument (ESA Sentinel-2): from the diffuser procurement until the test instrument at CSL. In MSI Instrument (ESA Sentinel-2): from the diffuser procurement until the test instrument at CSL. |
Jamotton, P., Domken, I., Marquet, B. (Other coll.), Liébecq, S. (Other coll.), Grodent, C. (Other coll.), & Cucchiaro, A. (Other coll.). (2010). Developments done at CSL for the testing of Herschel Telescope and Instruments of the Planck Reflectors and Spacecraft. In Developments done at CSL for the testing of Herschel Telescope and Instruments of the Planck Reflectors and Spacecraft. |
Jamotton, P., Liébecq, S. (Other coll.), Grodent, C. (Other coll.), & Cucchiaro, A. (Other coll.). (2010). JWST NIRSpec TMA cryogenic testing in CSL premises. In JWST NIRSpec TMA cryogenic testing in CSL premises. |
Ninane, N., Jung, P., Grodent, C. (Other coll.), Jamotton, P. (Other coll.), Tychon, I. (Other coll.), Liébecq, S. (Other coll.), & Cucchiaro, A. (Other coll.). (2007). Herschel Telescope Thermal Testing in CSL Focal 6,5 Chamber. In Herschel Telescope Thermal Testing in CSL Focal 6,5 Chamber. |
Domken, I., Bonnet, E. (Other coll.), Jamotton, P. (Other coll.), Franco, P. (Other coll.), Grodent, C. (Other coll.), Liébecq, S. (Other coll.), Thome, M. (Other coll.), Tychon, I. (Other coll.), & Cucchiaro, A. (Other coll.). (2006). Planck S/C thermal testing in Focal 5 facility. In Planck S/C thermal testing in Focal 5 facility. |
Ninane, N., Jung, P., Grodent, C. (Other coll.), Jamotton, P. (Other coll.), Tychon, I. (Other coll.), Liébecq, S. (Other coll.), & Cucchiaro, A. (Other coll.). (2006). Herschel Telescope Thermal Testing in CSL Focal 6,5 Chamber. In Herschel Telescope Thermal Testing in CSL Focal 6,5 Chamber. |
Jamotton, P., Cucchiaro, A. (Other coll.), Delrée, C. (Other coll.), & Liébecq, S. (Other coll.). (2004). Measurement of the absorptance-emittance of black paint surfaces at temperatures from 10 to 120 [K]. In Measurement of the absorptance-emittance of black paint surfaces at temperatures from 10 to 120 [K]. |