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Regulatory Approach for Nuclear Thermal PropulsionNuclear Thermal Propulsion (NTP) is being developed to support crewed or cargo transfer missions to Mars. Obtaining regulatory approval for NTP engine testing proves a challenge for not only the technology maturation required but also the fabrication, launch and operational nuclear regulatory environments. Existing regulations currently apply to either (1) high power, long duration commercial power plants, or (2) low power, short duration research reactors. NTP systems find themselves in a separate and unique area due to their higher power but short operating duration. This is supplemented by use of the reactor coolant as propellant. When planning the regulatory approach for NTP systems, operations in space and testing on Earth must be considered – each have their own challenges. This paper identifies a preliminary pathway for regulatory approval to operate a NTP demonstration engine as well as supporting test data that is recommended to be generated during the development program to support major regulatory milestones and deliverables.
Document ID
20230005415
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Alexander Pingel
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
James Werner
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Alexander Foutch
(Missouri University of Science and Technology Rolla, Missouri, United States)
Date Acquired
April 13, 2023
Subject Category
Spacecraft Propulsion and Power
Spacecraft Design, Testing and Performance
Meeting Information
Meeting: Nuclear and Emerging Technologies for Space (NETS)
Location: Idaho Falls, ID
Country: US
Start Date: May 7, 2023
End Date: May 11, 2023
Sponsors: American Nuclear Society
Funding Number(s)
CONTRACT_GRANT: 80LARC17C0003
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
Regulatory
Nuclear Thermal Propulsion
Nuclear Safety
Ground Testing
Environmental Impact
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