SKYHAVEN SYSTEMS, LLC — National Aeronautics and Space Administration SBIR Phase I: Z2

Description

nbsp;nbsp;nbsp;nbsp;nbsp; NASA is interested in more sophisticated thermal control technologies that can operate in severe environments with a wide range of heat loads. Effective heat rejection is needed for a number of NASA missions especially those associated with planetary and lunar orbits where extreme temperature differences due to lighted versus dark regions challenge radiator systems. Supplemental heat rejection systems are needed with these radiators to fully reject the heat loads from space vehicles. Phase change material (PCM) heat exchangers are capable of supplementing these radiators, especially for long duration missions. These systems store excess thermal energy during periods of high heat loads or hot thermal environments by melting a material within the heat exchanger. At a later time, this heat within the heat exchanger is removed freezing the phase change material. This frozen phase change material is thus capable of adsorbing a heat load again continuing the process.