2021
DOI: 10.1016/j.anucene.2020.107847
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Design research for the porous hexagonal prism shaped fuel element adopted in nuclear thermal propulsion reactor based on neutronics and thermal-hydraulics coupled method

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Cited by 12 publications
(3 citation statements)
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“…Uniaxial tension simulations were conducted for the fuel and the matrix, and the energy release rates (G c ) were adjusted iteratively until each material cracked at the correct fracture stress The phase-field fracture model was implemented using the finite element method with the Multiphysics Object-Oriented Simulation Environment (MOOSE), 38 as was done with the original model. 1 The J2 plasticity model in MOOSE was used to describe the constitutive behavior. Implicit time integration was used in the model.…”
Section: Materials Properties and Model Parametersmentioning
confidence: 99%
See 1 more Smart Citation
“…Uniaxial tension simulations were conducted for the fuel and the matrix, and the energy release rates (G c ) were adjusted iteratively until each material cracked at the correct fracture stress The phase-field fracture model was implemented using the finite element method with the Multiphysics Object-Oriented Simulation Environment (MOOSE), 38 as was done with the original model. 1 The J2 plasticity model in MOOSE was used to describe the constitutive behavior. Implicit time integration was used in the model.…”
Section: Materials Properties and Model Parametersmentioning
confidence: 99%
“…1. The gas also serves to cool the reactor, producing a temperature change in the axial direction of over 2000 K. 1 During operation, such a reactor would undergo multiple restart and short-burn propulsion cycles 2,3 for a combined burn time of under 2 h at very high temperature (2800 K to 3000 K). 2,4 In addition, the reactor may operate at low power and temperature between propulsion cycles to supply electrical power to the spacecraft 2,4 (hundreds of kW e to 1 MW e ).…”
Section: Introductionmentioning
confidence: 99%
“…The propellant flows through the subchannels of the fuel elements and absorbs thermal energy, producing an axial temperature difference exceeding 2000 K (Ref. 6). Then, the hightemperature hydrogen gas is exhausted through a nozzle and produces a reaction force that moves the rocket forward.…”
Section: Introductionmentioning
confidence: 99%