Datasets / Titanium Heat Pipe Thermal Plane Project


Titanium Heat Pipe Thermal Plane Project

Published By National Aeronautics and Space Administration

Issued over 9 years ago

US
beta

Summary

Type of release
a one-off release of a single dataset

Data Licence
Not Applicable

Content Licence
Creative Commons CCZero

Verification
automatically awarded

Description

Thermacore Inc. proposes an innovative titanium heat pipe thermal plane for passive thermal control of individual cells within a fuel cell stack. The proposed technology eliminates actively pumped liquid coolant loops, which improves system efficiency, reliability, safety, simplicity, life cycle as well as saves weight and volume. Although the main purpose for this technology is thermal management of fuel cells for space applications, the same technology can be applied for electronics cooling: heat spreaders and heat sinks, where thin design is required. The proposed titanium heat pipe thermal plane will be reliable passive heat transfer device with the following parameters: bulk density: under 3 grams per cubic centimeter, thickness: less than 0.050 inches, effective thermal conductivity: in excess of 2,000 W/(m K), electrical resistivity: less than 0.2 ohms-cm, operation against gravity: 4 inches