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Title: Assessment of Near-Term Fuel Screening and Qualification Needs for Nuclear Thermal Propulsion Systems

Abstract

Nuclear thermal propulsion (NTP) is an in-space propulsion technology capable of both high specific impulse (850–1000 s) and thrust (44–1112 kN), which can help reduce trip times for crewed missions beyond low Earth orbit. NTP technology has been demonstrated during historic programs. Over 20 ground test reactor experiments were performed, which demonstrated the prototypic reactor operations, during the Nuclear Engine for Rocket Vehicle Application (NERVA)/Rover program (1955–1972). Although historical programs have shown that NTP is a viable in-space propulsion technology, developing NTP in modern programs is contingent on the development and qualification of ultrahigh-temperature nuclear fuel technologies that can withstand engine operating conditions. In historical NTP development programs such as NERVA/Rover, prototypic reactor/engine schemes were ground tested to assess the overall system feasibility and to qualify the reactor fuel forms for eventual flight systems. Although this approach is effective to verify fuel performance under prototypic conditions, relying solely on full-scale NTP reactor tests as the pathway for verifying or qualifying fuel is inefficient and cost prohibitive today. Additionally, modern nuclear licensing requirements state that before test reactor approval, reactor components and fuel elements should be qualified via non-nuclear (out-of-pile) and nuclear (in-pile) testing under representative operating conditions. Using this methodology,more » fuel matures as production scale fabrication methods are established, and as produced fuel performance is demonstrated. Here, this paper provides an overview of historical approaches to NTP fuel performance maturation, including fuel screening and qualification needs, and provides insight for establishing an efficient testing paradigm that can be implemented to rapidly and affordably develop NTP fuel forms for eventual qualification.« less

Authors:
 [1]; ORCiD logo [2];  [2]
  1. Analytic Mechanics Associates, Huntsville, AL (United States); Univ. of Tennessee, Knoxville, TN (United States)
  2. Oak Ridge National Lab. (ORNL), Oak Ridge, TN (United States); Univ. of Tennessee, Knoxville, TN (United States)
Publication Date:
Research Org.:
Oak Ridge National Laboratory (ORNL), Oak Ridge, TN (United States)
Sponsoring Org.:
USDOE; National Aeronautics and Space Administration (NASA)
OSTI Identifier:
1657981
Alternate Identifier(s):
OSTI ID: 1656663
Grant/Contract Number:  
AC05-00OR22725; NNX15AQ35H
Resource Type:
Accepted Manuscript
Journal Name:
Nuclear Engineering and Design
Additional Journal Information:
Journal Volume: 367; Journal Issue: 1; Journal ID: ISSN 0029-5493
Publisher:
Elsevier
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING

Citation Formats

Palomares, Kelsa, Howard, Richard H., and Steiner, Tyler. Assessment of Near-Term Fuel Screening and Qualification Needs for Nuclear Thermal Propulsion Systems. United States: N. p., 2020. Web. doi:10.1016/j.nucengdes.2020.110765.
Palomares, Kelsa, Howard, Richard H., & Steiner, Tyler. Assessment of Near-Term Fuel Screening and Qualification Needs for Nuclear Thermal Propulsion Systems. United States. https://doi.org/10.1016/j.nucengdes.2020.110765
Palomares, Kelsa, Howard, Richard H., and Steiner, Tyler. Sat . "Assessment of Near-Term Fuel Screening and Qualification Needs for Nuclear Thermal Propulsion Systems". United States. https://doi.org/10.1016/j.nucengdes.2020.110765. https://www.osti.gov/servlets/purl/1657981.
@article{osti_1657981,
title = {Assessment of Near-Term Fuel Screening and Qualification Needs for Nuclear Thermal Propulsion Systems},
author = {Palomares, Kelsa and Howard, Richard H. and Steiner, Tyler},
abstractNote = {Nuclear thermal propulsion (NTP) is an in-space propulsion technology capable of both high specific impulse (850–1000 s) and thrust (44–1112 kN), which can help reduce trip times for crewed missions beyond low Earth orbit. NTP technology has been demonstrated during historic programs. Over 20 ground test reactor experiments were performed, which demonstrated the prototypic reactor operations, during the Nuclear Engine for Rocket Vehicle Application (NERVA)/Rover program (1955–1972). Although historical programs have shown that NTP is a viable in-space propulsion technology, developing NTP in modern programs is contingent on the development and qualification of ultrahigh-temperature nuclear fuel technologies that can withstand engine operating conditions. In historical NTP development programs such as NERVA/Rover, prototypic reactor/engine schemes were ground tested to assess the overall system feasibility and to qualify the reactor fuel forms for eventual flight systems. Although this approach is effective to verify fuel performance under prototypic conditions, relying solely on full-scale NTP reactor tests as the pathway for verifying or qualifying fuel is inefficient and cost prohibitive today. Additionally, modern nuclear licensing requirements state that before test reactor approval, reactor components and fuel elements should be qualified via non-nuclear (out-of-pile) and nuclear (in-pile) testing under representative operating conditions. Using this methodology, fuel matures as production scale fabrication methods are established, and as produced fuel performance is demonstrated. Here, this paper provides an overview of historical approaches to NTP fuel performance maturation, including fuel screening and qualification needs, and provides insight for establishing an efficient testing paradigm that can be implemented to rapidly and affordably develop NTP fuel forms for eventual qualification.},
doi = {10.1016/j.nucengdes.2020.110765},
journal = {Nuclear Engineering and Design},
number = 1,
volume = 367,
place = {United States},
year = {Sat Aug 29 00:00:00 EDT 2020},
month = {Sat Aug 29 00:00:00 EDT 2020}
}

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