Skip Navigation
SBIR/STTR

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

Light bulb

Suggest an Edit

Recommend changes and additions to this project record.

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.

^