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The Use of Immersion Rigs for High Temperature Hydrogen Exposure Testing Within the Nuclear Thermal Rocket Element Environmental Simulator (NTREES)The Nuclear Thermal Rocket Element Environmental Simulator (NTREES) was designed to perform non-nuclear testing of nuclear thermal rocket (NTR) fuel elements and materials. NTREES can simulate the thermal hydraulic environment within an NTR and has been leveraged to provide critical information on component performance and material compatibility. NTREES has the ability to expose test articles to pressurized Hydrogen gas up to 1000 psig and 225 g/s. NTREES tests are operated in a deoxygenated environment of Nitrogen or Argon pressurized up to 1000 psig. NTREES simulates fission heat through induction heating powered by a 1.2 MW AC power supply, and NTREES has recorded temperatures exceeding 3700K. To perform hot Hydrogen exposure tests on materials more rapidly and earlier in the fuel development process, NTREES must be able to test small material samples on the order of 1 square inch in volume, individual fuel assembly subcomponents, and particle materials. To meet these needs, multiple testing rigs have been developed to immerse test specimens in hot Hydrogen, with each "immersion rig" varying in its capability of sample type and performance range in order to meet the broadest range of testing needs. Herein is a discussion of a selection of these “immersion rigs.”
Document ID
20240013998
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Jacob O Ondeck
(Marshall Space Flight Center Redstone Arsenal, United States)
James W Post
(Marshall Space Flight Center Redstone Arsenal, United States)
Michael P Schoenfeld
(Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
November 5, 2024
Subject Category
Aircraft Propulsion and Power
Meeting Information
Meeting: Joint Army-Navy-NASA-Air Force (JANNAF) Subcommittee Meeting
Location: Charlotte, NC
Country: US
Start Date: December 9, 2024
End Date: December 13, 2024
Sponsors: Joint Army-Navy-NASA-Air Force (JANNAF) Interagency Propulsion Committee
Funding Number(s)
WBS: 039889.04.01.02.62
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Nuclear Thermal Propulsion
High Temperature Material Testing
Space Nuclear Propulsion
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