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In-Situ Heat Rejection to the Martian AtmosphereIn order to provide in-situ heat rejection to the thin Martian atmosphere, approaches relying on forced convection and buoyancy flow are conceptualized. A convective radiator concept utilizing a fan to draw local atmosphere through an expanded metal foam heat exchanger panel is developed. To provide a pumped fluid loop interface, flow tubes are embedded in the heat exchanger panel and heat is transferred from the tubes to the foam via conduction and subsequently convectively to the environment. To forgo the use of a specialized high throughput fan, a concept utilizing a buoyant chimney tower to draw atmospheric flow through a low pressure drop heat exchanger is also considered. Both concepts may best align with moderate- to high-temperature heat loads that provide a significant delta temperature relative to the ambient atmosphere temperature. While eliminating dust accumulation on radiator surfaces, some type of serviceable filtration or screening may be required to prevent accumulation of dust inside the expanded metal foam heat exchanger for both concepts.
Document ID
20260007919
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
R Gregory Schunk
(Amentum Chantilly, Virginia, United States)
Date Acquired
August 17, 2026
Subject Category
Fluid Mechanics and Thermodynamics
Engineering (General)
Meeting Information
Meeting: 37th Thermal and Fluids Analysis Workshop (TFAWS)
Location: Huntsville, AL
Country: US
Start Date: August 31, 2026
End Date: September 4, 2026
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
CONTRACT_GRANT: 954879.06.03.14.62
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Heat Rejection
Buoyancy
Forced Convection
Martian
Mars
Radiator
Thermal
Spacecraft
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