Small Spacecraft Technology
Small Spacecraft Integrated Power System with Active Thermal Control
Project Description
This project will develop an integrated power generation and energy storage system with an active thermal management system. Carbon fiber solar panels will contain microvascular fluid channels, and provide battery cooling and a cold plate for other satellite devices. The system is scalable from 6U CubeSats up to 100 kg small satellites.
More »Anticipated Benefits
This project will significantly increase the capabilities of deep space CubeSats, allowing more powerful and hotter spacecraft systems than are currently available with state of the art commercial systems. This new system will fulfill the needs of upcoming NASA cislunar missions and beyond.
More »Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
| University of Illinois at Urbana-Champaign | Lead Organization | Academia | Urbana, Illinois |
Ames Research Center
(ARC)
|
Supporting Organization | NASA Center | Moffett Field, California |
Primary U.S. Work Locations
-
California
-
Illinois
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