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Thermal Cycle and Capacitance Testing of Mezzo Industries Phase Change Material Heat CapacitorA phase change material heat capacitor prototype, designed and built under a NASA Small Business Innovation Research grant by Mezzo Technologies, was tested through coolant thermal cycling within the expected flow rates and temperature range of the Orion spacecraft’s propylene glycol-water mixture coolant system. Testing was performed with the phase change material contained under sealed conditions after a degassing procedure and exposed to atmosphere without prior degassing. The useful heat storage capacitance was measured and compared to Orion spacecraft requirements and theoretical N-Pentadecane storage capacity.
Document ID
20260005518
Acquisition Source
Johnson Space Center
Document Type
Presentation
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) Chantilly, France)
Date Acquired
June 16, 2026
Subject Category
Fluid Mechanics and Thermodynamics
Meeting Information
Meeting: 55th International Conference on Environmental Systems (ICES)
Location: Rio Grande
Country: PR
Start Date: July 12, 2026
End Date: July 16, 2026
Sponsors: Collins Aerospace (United States)
Funding Number(s)
WBS: 374409.06.02.10.05
CONTRACT_GRANT: 80JSC022DA035
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
Propylene Glycol Water
N-pentadecane
Laser Welding
Mezzo Technologies
Orion
Thermal Control System
Phase Change Material
Heat capacitor
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