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Development of an Additively Manufactured Subscale Secondary Sealed Container for the NASA FROSTE ProjectThis presentation details the development of an additively manufactured (AM) subscale test article for the secondary sealed container (SSC) as part of the NASA FROSTE project. FROSTE is focused on the collection of regolith samples from shadowed regions of the Moon and the preservation of those samples at cryogenic temperatures for return to Earth. Our team was integrated into the FROSTE program to leverage innovative design approaches and additive manufacturing capabilities in support of a scalable development strategy, where the subscale configuration serves as the development path toward a full-scale SSC.

Scalmalloy was selected as the primary material for all AM components due to its favorable strength-to-weight ratio, thermal conductivity, and demonstrated performance in aerospace applications. Its aluminum-based composition supports robust mechanical behavior at cryogenic temperatures while enabling efficient heat transfer and control of thermal gradients within the containment system.

The SSC architecture consists of an outer container assembly that houses a phase change material (PCM) tank, which in turn contains primary containers holding the regolith. Thermal management relies on controlled conductive and radiative heat transfer, including a thermal connection assembly that interfaces the PCM tank to an external cryocooler via a thermal strap, and IMLI surrounding the PCM tank to inhibit radiative heat transfer. The outer container assembly incorporates sealing interfaces, thermal connection ports, and I/O feedthroughs, with PTFE spring seals used at critical interfaces to maintain containment integrity.

The PCM tank is manufactured as a single monolithic Scalmalloy component and incorporates an integral lattice structure to minimize thermal gradients, internal channels for thermocouple routing, and interface features for thermal connection assembly integration. The tank is centrally suspended within the outer container using support rings, with G10 insulating components employed to inhibit thermal leaks. This work describes the design methodology, AM approach, and key considerations used to inform the design.
Document ID
20260004465
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Melissa Susan Forton
(Quadrus Corporation Redstone Arsenal, United States)
Collin James Adair
(Quadrus Corporation)
Blake Hyla
(Quadrus Corporation)
Ryan Anderson
(Quadrus Corporation)
Joseph D Sims
(Quadrus Corporation)
Date Acquired
May 19, 2026
Subject Category
Mechanical Engineering
Lunar and Planetary Science and Exploration
Meeting Information
Meeting: National Space and Missile Materials Symposium (NSMMS)
Location: Columbia, SC
Country: US
Start Date: June 22, 2026
End Date: June 25, 2026
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
WBS: 648295.05.01.62
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
regolith
lunar samples
cryogenic conditioning
cryogenic samples
curation
collection
planetary science
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