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Coupled Reactor and Engine Nuclear Thermal Propulsion Modeling Methodology The design and development process of a Nuclear Thermal Propulsion (NTP) system requires extensive multiphysics modeling to couple the neutron physics and thermal feedback effects to determine the reactor’s power shape. Propulsion system performance codes utilize this power shape to determine NTP key performance parameters. While the power shape is heavily dependent on the temperature profile and geometry of the reactor, many analyses either assume a constant power shape, or use neutronics analysis to determine a power shape for a specific reactor configuration. The development of a coupling interface for a propulsion system performance code and a Monte Carlo neutron transport code (OpenMC) allows for the reactor power shape to be calculated in a Picard iteration.
Document ID
20230016865
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Jacob Stonehill
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Daria Nikitaeva
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Corey Smith
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Matthew Duchek
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Date Acquired
November 17, 2023
Subject Category
Spacecraft Propulsion and Power
Meeting Information
Meeting: Nuclear and Emerging Technologies for Space (NETS)
Location: Santa Fe, NM
Country: US
Start Date: May 6, 2024
End Date: May 10, 2024
Sponsors: American Nuclear Society
Funding Number(s)
CONTRACT_GRANT: 80LARC23DA003
Distribution Limits
Public
Copyright
Public Use Permitted.
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