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A thermal‐hydraulic model of an open‐cycle gas core nuclear rocket is developed. The two‐dimensional Navier‐Stokes equations, the energy equation, and the species diffusion equation are solved for high temperature two‐species gas flow. A description of the model and the method of solution is presented, as well as the results for a cylindrical gas core reactor design. The results provide valuable insight into the fluid flow and species mixing within an open‐cycle gas core nuclear rocket

A Comprehensive Thermal-Hydraulic Model of an Open-Cycle Gas Core Nuclear Rocket