Active CryoCubeSat

Swenson, Charles

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NASA NTRS · 20160007914

Active CryoCubeSat

Swenson, Charles

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Abstract

The Active CryoCubeSat project will demonstrate an advanced thermal control system for a 6-Unit (6U) CubeSat platform. A miniature, active thermal control system, in which a fluid is circulated in a closed loop from thermal loads to radiators, will be developed. A miniature cryogenic cooler will be integrated with this system to form a two-stage thermal control system. Key components will be miniaturized by using advanced additive manufacturing techniques resulting in a thermal testbed for proving out these technologies. Previous CubeSat missions have not tackled the problem of active thermal control systems nor have any past or current CubeSat missions included cryogenic instrumentation. This Active CryoCubeSat development effort will provide completely new capacities for CubeSats and constitutes a major advancement over the state-of-the-art in CubeSat thermal control.

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CubeSat Cryocooler Active thermal control

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BibTeX RIS

Swenson, Charles. 2016-04-20. Active CryoCubeSat. https://ntrs.nasa.gov/citations/20160007914

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