Aufbau eines Versuchsstandes für den ECH Upper Launcher in ITER - Schlussbericht zum Vorhaben 3FUS0010 (KIT Scientific Reports ; 7694)

Um Plasmainstabilitäten zu begegnen, werden in vier der oberen Ports im ITER Vakuumgefäß Electron Cyclotron Launcher installiert. Diese bestehen im Wesentlichen aus einer trapezförmigen Stahlkonstruktion, welche die Mikrowellenkomponenten (im Wesentlichen Spiegel und Wellenleiter) beherbergt. Bei der Konstruktion eines solchen Launchers müssen als wesentliche Vorgaben die mechanische Festigkeit, die ausreichende Kühlung des Systems und wirksame Abschirmung gegen Neutronen berücksichtigt werden

Response to Comment on “Maxima in the thermodynamic response and correlation functions of deeply supercooled water”

Caupin et al. have raised several issues regarding our recent paper on maxima in thermodynamic response and correlation functions in deeply supercooled water. We show that these issues can be addressed without affecting the conclusion of the paper.113Ysciescopu

The ITER EC H&CD Upper Launcher: Analysis of vertical Remote Handling applied to the BSM maintenance

This paper deals with Remote Handling activities foreseen on the Blanket Shield Module, the plasma facing component of the ITER Electron Cyclotron Heating and Current Drive Upper Launcher. The maintenance configuration considered here is the Vertical Remote Handling, meaning gravity acting along the launcher radial axis. The plant, where the maintenance under consideration is occurring, is the Hot Cell Facility Work Cell. The study here reported has been carried out within the presently ongoing EFDA Goal Oriented Training program on Remote Handling (GOT-RH), which aims to support ITER activities. This document and its contents have to be considered as part of a more vast RAMI analysis to be developed within the GOT-RH, which aims to maximize the Electron Cyclotron Heating and Current Drive system availability. The Baseline CAD model of the Electron Cyclotron Heating and Current Drive Upper Launcher is currently in its preliminary design phase and does not provide enough details for developing a fully detailed maintenance strategy. Therefore, through a System Engineering approach, a set of assumptions was conceived on the launcher structure, as a basis for development of a Remote Handling strategy. Moreover, to compare different design solutions related to the possibility of integrating a quasi-optical component into the Blanket Shield Module, a Trade-Off was made, and its contents are shown here. The outcome of this System Engineering approach has been formalized into Task Definition Forms whose contents are reported here. The Remote Handling strategy presented in this work will be tested in the near future both through Virtual Reality simulations and through prototype experiments