Skip Navigation

Highly Efficient and Robust Micropump for Small Spacecraft Thermal Control, Phase I

Completed Technology Project

Project Introduction

Highly Efficient and Robust Micropump for Small Spacecraft Thermal Control, Phase I
With the introduction of low-cost, small, rapidly configurable spacecraft, the need for robust, versatile, readily deployable, and easily ground-testable thermal control technologies becomes ever more critical. Passive two-phase thermal control technology, that is, heat pipes, defines the current state-of-the-art, yet it is clear that this technology alone will not meet the needs of future spacecraft. Dramatic improvements in the versatility and effectiveness of heat pipes are possible with a small amount of mechanical pumping assistance. With the separation of the liquid pumping and heat transfer functions, greater design freedom and system optimization is also afforded. However, before pump-assisted heat pipes can become a viable alternative, significant improvement in pump lifetime and robustness is needed. Lynntech proposes to develop a long-life, robust, low-power, high pressure-rise, electrochemically-driven micropump for use in pump-assisted heat pipes. More »

Primary U.S. Work Locations and Key Partners

Project Library

Share this Project

Organizational Responsibility

Project Management

Project Duration

This is a historic project that was completed before the creation of TechPort on October 1, 2012. Available data has been included. This record may contain less data than currently active projects.

A final report document may be available for this project. If you would like to request it, please contact us.