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Thermal Cycle and Capacitance Testing of Mezzo Industries Phase Changer Material Heat CapacitorEffective Thermal management is essential for the safety and performance of human spacecraft, especially during long-duration missions with fluctuating heat loads. Phase Change Material (PCM) heat exchangers offer a compact, efficient solution by storing and
releasing thermal energy through latent heat during phase transitions. This allows PCM systems to buffer transient thermal loads without immediate heat rejection, reducing the need for oversized radiators – particularly critical during ascent and re-entry when radiators are stowed. By maintaining stable temperatures in crew cabins and equipment bays, PCM technology enhances crew comfort, protects sensitive systems, and supports long-term mission sustainability with minimal mass and volume impact. A phase change material heat capacitor prototype, designed and built under a NASA Small Business Innovation Research grant by Mezzo Technologies, utilizes a laser welding microtube manufacturing process that promises increased reliability and performance over current manufacturing methods like brazing. This heat exchanger was tested through coolant thermal cycling within the expected flow rates and temperature range of the Orion spacecraft, the crewed spacecraft taking NASA astronauts to the moon under the Artemis Program. The useful heat storage capacitance was measured and compared to Orion spacecraft requirements.
Document ID
20260003053
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Michael C Johnston
(Johnson Space Center Houston, United States)
Jon-Michael Tucker
(Johnson Space Center Houston, United States)
Ryan P Dippolito
(Johnson Space Center Houston, United States)
Priscilla Nizio
(Johnson Space Center Houston, United States)
Ian Anchondo
(Johnson Space Center Houston, United States)
Dongeun Lee
(Amentum (United States) Houston, Texas)
Date Acquired
April 13, 2026
Publication Date
July 12, 2026
Publication Information
Publisher: International Conference on Environmental Systems
Subject Category
Spacecraft Design, Testing and Performance
Report/Patent Number
ICES-2026-522
Meeting Information
Meeting: 55th International Conference on Environmental Systems (ICES)
Location: Rio Grande, PR
Country: US
Start Date: July 12, 2026
End Date: July 16, 2026
Sponsors: International Conference on Environmental Systems
Funding Number(s)
CONTRACT_GRANT: 80JSC022DA035
CONTRACT_GRANT: 80TECH22DA002
WBS: 374409.06.02.10.05
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
Active Thermal Control Systems
Propylene Glycol Water
N-Pentadecane
Laser Welding
Mezzo Technologies
Orion
Thermal Control System
Phase Change Material
Heat Exchanger
Heat Capacitor
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