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 |
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 |
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. |
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 |