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The Use of Immersion Rigs for High Temperature Hydrogen Exposure Testing Within the Nuclear Thermal Rocket Element Environmental Simulator (NTREES): NTREES-5 Hydrogen Heat Exchanger (N5HHX-01)The Nuclear Thermal Rocket Element Environmental Simulator (NTREES) facility at NASA’s Marshall Space Flight Center (MSFC) subjects materials and components typically found on nuclear thermal propulsion (NTP) systems to non-nuclear simulations of prototypic NTP reactor thermohydraulic environments. With 1.2 MW of inductive power available, the currently employed methods to simulate nuclear heating in NTREES consist of 1) inductively heating a test specimen, which typically cannot be performed on ceramic materials, or 2) heating gas that envelops the test specimen. The latter of these has provided a basis for developing so-called “immersion rigs” to be used in NTREES. Furthermore, immersion rigs are especially useful in the case of smaller, technically challenging test specimens.

One such device, the “NTREES-5 Hydrogen Heat Exchanger” (N5HHX-01), designed and deployed to test small material coupons to ~0.5 g/s of 2800 K, 500 psi Hydrogen, is discussed herein. To achieve this desired delivery temperature level, the most suitable material for the N5HHX’s construction was pure tungsten, which imposed budgetary and manufacturing challenges. Also discussed in this paper is the design of the N5HHX rig’s sample container, which became the first iteration of improving NTREES small material coupon test operations by permitting rapid changeout of different material samples.
Document ID
20260003496
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 27, 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)
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
Reactor Testing
High Temperature Materials Testing
Nuclear Thermal Propulsion
Space Nuclear Propulsion
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