Small Business Innovation Research/Small Business Tech Transfer
Modified Ionic Liquids for Thermal Properties in CubeSats, Phase I
Project Introduction
NASA desires new phase change systems to regulate heat transfer among components within a CubeSat small spacecraft. The temperature variation within the small spacecraft often leads to large temperature spikes that may be detrimental to onboard unit components. Temperatures can often range from -40°C to +80°C. InnoSense LLC (ISL) will develop an ionic liquid-based heat transfer fluid for use within the CubeSat. Our method will be to control the functional groups attached to an ionic liquid to tune the melting point and reduce electrical conductivity of the material. The proposed technology will be tailored for use with a variety of different components within the CubeSat. In Phase I, ISL proposes to synthesize a functionalized ionic liquid and test its thermal properties. The proposed material is expected to have high thermal conductivity, high heat storage density, and melting point with range of component operation. During Phase II and follow-on phases, the proposed technology will be refined, optimized, and scaled to larger size production. The proposed materials will also be tested in various environments. Packaging methods will be investigated and the final product will be integrated into working CubeSats with the assistance of a CubeSat design company.
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Anticipated Benefits
As spacecraft's size reduces, damage resulting from the effect of thermal fluctuations becomes increasingly detrimental. When components turn on and off, the temperature of the spacecraft interior can rapidly rise, damaging critical components. By including a phase change material that can be integrated into a variety of components, shapes and orientations, the temperature of the spacecraft can be readily regulated. Through such temperature regulations, critical device components will be maintained at optimum operational temperatures. Commercial uses of the proposed ionic liquid heat transfer fluid will include extreme environment vehicles. The performance of these vehicles will be improved by the addition the ionic liquid phase change material that will regulate internal temperatures, reducing energy use within the vehicle. This will, in turn, also reduce the size of heat exchangers leading to more open, workable space within the shelter or vehicle.
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Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
| Innosense, LLC | Lead Organization |
Industry
Minority-Owned Business,
Small Disadvantaged Business (SDB),
Women-Owned Small Business (WOSB)
|
Torrance, California |
Marshall Space Flight Center
(MSFC)
|
Supporting Organization | NASA Center | Huntsville, Alabama |
Primary U.S. Work Locations
-
Alabama
-
California
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Organizational Responsibility
Responsible Mission Directorate:
- Space Technology Mission Directorate (STMD)
Lead Organization:
- Innosense, LLC
Responsible Program:
- Small Business Innovation Research/Small Business Tech Transfer
Project Management
Project Duration
Start: Jun 2015
End: Dec 2015
Technology Maturity (TRL)
| Start: | 2 |
| Current: | 4 |
| Estimated End: | 4 |
Applied Research
Development
Demo & Test
Technology Areas
Primary:
- TX14 Thermal Management Systems
- TX14.2 Thermal Control Components and Systems
- TX14.2.2 Heat Transport
Target Destination
Earth
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