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NaK release model for MASTER-2009
Authors:Carsten Wiedemann  Sven Flegel  Johannes Gelhaus  Holger Krag  Heiner Klinkrad  Peter Vörsmann
Affiliation:1. Institute of Mechanics, Materials and Civil engineering, Université catholique de Louvain, Louvain-la-Neuve 1348, Belgium;2. Department of Mechanical Engineering, Vrije Universiteit Brussel, Brussels 1050, Belgium;3. BURN Joint Research Group, Vrije Universiteit Brussel & Université Libre de Bruxelles, Brussels, Belgium;4. Energy Systems Division, Argonne National Laboratory, Argonne, IL 60439, USA;5. Physico-Chimie des Processus de Combustion et de l’Atmosphère (PC2A), Université Lille 1 Sciences et Technologies, Cité Scientifique, Villeneuve d’Ascq Cedex 59655, France
Abstract:Sodium–potassium droplets from the primary coolant loop of Russian orbital reactors have been released into space. These droplets are called NaK droplets. Sixteen nuclear powered satellites of the type RORSAT launched between 1980 and 1988 activated a reactor core ejection system, mostly between 900 and 950 km altitude. The core ejection causes an opening of the primary coolant loop. The liquid coolant consists of eutectic sodium–potassium alloy and has been released into space during these core ejections. The NaK coolant has been forming droplets up to a diameter of 5.5 cm. NaK droplets have been modeled before in ESA's MASTER Debris and Meteoroid Environment Model. The approach is currently revised for the MASTER-2009 upgrade. A mathematical improvement is introduced by substituting the current size distribution function by the modified Rosin–Rammler equation. A bimodal size distribution is derived which is based on the modified mass based Rosin–Rammler equation. The equation is modified by truncating the size range and normalizing over the finite range between the size limits of the smallest and the biggest droplet. The parameters of the model are introduced and discussed. For the validation of the NaK release model, sixteen release events are simulated. The resulting size distribution is compared with radar measurement data. The size distribution model fits well with revised published measurement data of radar observations. Results of orbit propagation simulation runs are presented in terms of spatial density.
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