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Coupled Reactor Multiphysics and Mass Scalability Assessment for Crewed Megawatt-Class NEP System ArchitecturesNuclear Electric Propulsion (NEP) is an in-space propulsion technology capable of enabling opposition and conjunction class crewed Mars missions. NEP subsystems include the reactor for heat generation, a power conversion system (PCS), power management and distribution, electric propulsion system, and heat rejection system. Specific mass, or α (kg/kWe), is a key performance parameter (KPP) of the propulsion system which is directly scalable with the performance and mass predictions for each individual component. To inform technology maturation planning activities, full system and component level parametric modeling is ongoing to explore the design trade space and illustrate the effect of subsystem design choices on the system KPPs.

In this study, scaling of high-assay, low-enriched uranium reactor designs is assessed through coupled reactor physics and thermal hydraulics analyses. Scaling analyses evaluate the impact of system performance parameters (power level, interface temperatures) on mass for direct gas cooled, pumped liquid metal, and passively-cooled heat pipe reactor concepts. Each concept requires specific geometries, fluids, and power conversion interface conditions (temperature, pressure, flow rate) to meet desired performance and mass. The reactor assembly includes the active core (fuel, moderator, cladding, working fluid), axial and radial neutron reflectors, control drums, structural support / pressure vessel, and external radiation shielding. Each of these components are parametrically sized based on performance parameters for a megawatt-class power cycle.

Results of this scaling analysis increase NEP propulsion system modeling fidelity and ultimately aim to support concept down-selection along with related technology development planning. The reactor and shield α are a function of several PCS and heat rejection system design choices, and reactor scaling with these parameters must be considered to enable an informed decision on an optimal reactor geometry and working fluid combination.
Document ID
20220017245
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Corey Smith
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Dennis Nikitaev
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Matthew Duchek
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Kelsa Palomares
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
DV Rao
(Los Alamos National Laboratory Los Alamos, New Mexico, United States)
Date Acquired
November 16, 2022
Subject Category
Spacecraft Propulsion and Power
Meeting Information
Meeting: Joint Army-Navy-NASA-Air Force (JANNAF) Subcommittee Meeting
Location: Huntsville, AL
Country: US
Start Date: December 5, 2022
End Date: December 9, 2022
Sponsors: United States Air Force, United States Army, United States Department of the Navy, National Aeronautics and Space Administration
Funding Number(s)
CONTRACT_GRANT: 80LARC17C0003
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Professional Review
Keywords
Nuclear Electric Propulsion
NEP
Reactor
Modeling & Simulation
Scalability
Heat Pipe
Gas-Cooled
Liquid Metal Cooled
Specific Mass
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