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U.S. Department of Energy
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HERMITE: a multi-dimensional space-time kinetics code for PWR transients

Technical Report ·
OSTI ID:7277302
The HERMITE space-time kinetics computer code is described. This code was developed for the analysis of design and off-design transients in large PWR's by means of a numerical solution to the multi-dimensional, few-group, time-dependent neutron diffusion equation including feedback effects of fuel temperature, coolant temperature, coolant density and control rod motion. The time-dependent neutron diffusion equation is solved by a finite element method. The heat conduction equation in the pellet, gap and clad is solved by a finite difference method. Continuity and energy conservation equations are solved for the coolant enthalpy and density. Extensive verification calculations have been performed and are summarized. HERMITE was applied to the three-dimensional analysis of the control element assembly ejection incident, and results were compared to the corresponding two-dimensional analysis. An input description is included as an appendix.
Research Organization:
Combustion Engineering, Inc., Windsor, CT (USA)
OSTI ID:
7277302
Report Number(s):
CENPD-188
Country of Publication:
United States
Language:
English