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MOPLR062 |
European Spallation Source (ESS) Normal Conducting Front End Status Report |
274 |
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- W. Wittmer, P.O. Gustavsson, F. Hellström, G. Hulla
ESS, Lund, Sweden
- I. Bustinduy, P.J. González, G. Harper, S. Varnasseri, C. de la Cruz
ESS Bilbao, Zamudio, Spain
- L. Celona, S. Gammino, L. Neri
INFN/LNS, Catania, Italy
- A.C. Chauveau, D. Chirpaz-Cerbat
CEA/IRFU, Gif-sur-Yvette, France
- F. Grespan, A. Pisent
INFN/LNL, Legnaro (PD), Italy
- P. Mereu
INFN-Torino, Torino, Italy
- O. Midttun
University of Bergen, Bergen, Norway
- O. Piquet, B. Pottin
CEA/DSM/IRFU, France
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The European Spallation Source (ESS) will deliver first protons on target by mid 2019. Civil construction of the accelerator tunnel has made good progress and will allow starting installation of the normal conducting frond end (NCFE) by end of 2017. To achieve these milestones the design of all major beam line components have been completed and the construction of the subsystems begun. We report on the advancement of the subsystems and the commissioning progress of the microwave discharge Proton Source (PS-ESS).
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Poster MOPLR062 [1.396 MB]
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DOI • |
reference for this paper
※ https://doi.org/10.18429/JACoW-LINAC2016-MOPLR062
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THPLR066 |
Preparation and Installation of IFMIF-EVEDA RFQ at Rokkasho Site |
1005 |
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- E. Fagotti, L. Antoniazzi, A. Baldo, A. Battistello, P. Bottin, L. Ferrari, M.G. Giacchini, F. Grespan, M. Montis, A. Pisent, D. Scarpa
INFN/LNL, Legnaro (PD), Italy
- D. Agguiaro, A.G. Colombo, A. Pepato, L. Ramina
INFN- Sez. di Padova, Padova, Italy
- F. Borotto Dalla Vecchia, G. Dughera, G. Giraudo, E.A. Macri, P. Mereu, R. Panero
INFN-Torino, Torino, Italy
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The IFMIF-EVEDA RFQ is composed of 18 modules for a total length of 9.8 m and is designed to accelerate the 125 mA D+ beam up to 5 MeV at the frequency of 175 MHz. The RFQ is subdivided into three Super-Modules of six modules each. The Super-Modules were pre-assembled, aligned and vacuum tested at INFN-LNL and then shipped to Rokkasho (Japan). At Rokkasho site a series of test were performed in order to verify the effect of the shipment on the cavity. The assembly debug, shipment equipment and the sequence of operations are described in this paper.
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DOI • |
reference for this paper
※ https://doi.org/10.18429/JACoW-LINAC2016-THPLR066
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