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The Use of Immersion Rigs for High Temperature Hydrogen Exposure Testing within the Nuclear Thermal Rocket Element Environmental Simulator (NTREES): Thermal Soak Rig (TSR)The Nuclear Thermal Rocket Element Environmental Simulator (NTREES) facility was purpose constructed to perform non-nuclear evaluations of nuclear thermal propulsion (NTP) system fuel materials and structures within prototypic thermochemical environments. This system has been utilized steadily in its ability to subject test specimens to thermochemical and thermohydraulic environments simulating that of an operating nuclear rocket engine. Fission heat is simulated by induction power and experiments are conducted within a ~1000 psi pressure vessel. Hydrogen is conventionally passed through the heated fuel surrogate test specimen while pressure, temperature, and gas species data are collected at various points along the experiment. In order to test fuel and material coupon samples, a class of test apparatus named “immersion rigs” are being developed and employed to more rapidly test these smaller and more technically challenging test specimen.

One example of a promising potential fuel structure, Tristructural-isotropic (TRISO) particles, presents unique challenges for testing of this type. TRISO fuel micro-particles are spheroids typically on the order of 500 – 1000 μm in diameter, and exposing a batch sample to hot hydrogen requires purpose-built special test equipment. Thusly, an immersion rig was developed and successfully demonstrated to expose ~1 g of micro-particles to hydrogen gas at temperatures and pressures relevant to NTP systems for the purpose of fuel evaluation. The rig, comprised primarily of graphite and pure tungsten, houses in its core a batch of micro-particles between pucks of porous silicon carbide (SiC). This approach permits gas flow while simultaneously retaining the particles in place. Herein is a discussion of the design, analysis, fabrication, and testing of the NTREES Thermal Soak Rig (TSR).
Document ID
20260003458
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Jacob Ondeck
(Marshall Space Flight Center Redstone Arsenal, United States)
James Post
(Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
April 24, 2026
Subject Category
Spacecraft Propulsion and Power
Meeting Information
Meeting: JANNAF June 2026 Meeting
Location: Pittsburgh, PA
Country: US
Start Date: June 1, 2026
End Date: June 4, 2026
Sponsors: Joint Army-Navy-NASA-Air Force (JANNAF) Interagency Propulsion Committee
Funding Number(s)
WBS: 907324.07.01.04.62
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
Space Nuclear Propulsion
Nuclear Thermal Propulsion
High Temperature Materials Testing
Reactor Testing
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