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Small Spacecraft Technology

Small Spacecraft Integrated Power System with Active Thermal Control

Completed Technology Project

Project Introduction

Small Spacecraft Integrated Power System with Active Thermal Control
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

Primary U.S. Work Locations and Key Partners

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Project Duration

Technology Maturity (TRL)

Technology Areas

Target Destinations

Light bulb

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