Aerogel-Based Super-Insulation



 The Aerogel-Based Super-Insulation was developed by Aspen Systems, Inc., of Marlborough, Massachusetts. This technology was developed under a NASA Small Business Innovation Research (SBIR) contract for KSC. This superinsulation is an innovative, flexible cryogenic insulation with extremely low thermal conductivity. The design of this product takes advantage of the low thermal conductivity of the ultralow-density aerogels (ULDAís) and incorporates a flexible, durable matrix to maximize applicability. The core of the superinsulation technology is aerogels formed at the fiber-fiber contacts, forcing solid heat transfer to occur through the aerogels. This configuration both improves the ease of handling aerogels and reduces the heat transfer rate through the fiber materials. The close-packed structure of aerogels also eliminates the open structures in the fiber matrix and, thereby, minimizes convection heat transfer. Therefore, improved thermal resistance can be achieved for both evacuated and nonevacuated systems while maintaining good flexibility. In addition, by producing the aerogels in an opacified fiber matrix, the structure also significantly inhibits radiation heat transfer in the infrared range. This technology can be easily adapted to a broad range of commercial applications.


Potential Commercial Uses Include 


Advantages 

The basic form of the super-insulation system is a blanket composed of aerogel-based radiation shield layers and low thermal conductivity aerogel/fiber matrix composites. The final product can be a blanket, sheet, sleeve, or clamshell unit, depending on the application (see the photograph). The blanket alone can be employed as an alternative to multilayer insulation or perlite powder in vacuum-jacketed systems. The configurations of the sheet and sleeve units are similar to the blanket but add outer skin and backing material. The outer skin provides (1) a weather barrier to prevent condensation of moisture or air, (2) safety and strength during handling and installation, and (3) durability for protection from harsh environments. The configuration of the clamshell unit is similar to that of the sheet or sleeve but is custom-sized to piping, pipe flange, or piping components (see the drawing). In this case, the superinsulation can be relatively rigid (not brittle) for insulating simple objects such as piping or can be flexible for insulating complex-shaped objects.

The thermal performance of the aerogel-based superinsulation has been measured by both transient heat flux and liquid nitrogen boiloff methods. The apparent thermal conductivity of the plain blanket super-insulation is lower than 1 milliwatt per meter-kelvin (R-value per inch greater than 140) at high vacuum (below 10E-5 torr) with cold and warm boundary temperatures of 77 and 280 kelvin. Most importantly, the thermal conductivity has been shown to be insensitive to residual gas pressure up to a vacuum level of 10E-1 torr. The thermal conductivity in ambient pressure nitrogen is below 10 milliwatts per meter-kelvin (R-value per inch greater than 14). Currently, Aspen Systems is producing aerogel thermal insulation products for a variety of customers. Prototype super-insulation systems are being field tested at KSC.


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Disclaimers
Disclaimer of Endorsement: Reference herein to any specific commercial products, process, or service by trade name, trademark, manufacturer, or otherwise, does not constitute or imply its endorsement, recommendation, or favoring by the United States Government. The views and opinions of authors expressed herein do not necessarily state or reflect those of the United States Government, and shall not be used for advertising or product endorsement purposes. 

Disclaimer of Liability: With respect to this multimedia document, neither the United States Government nor any of their employees, makes any warranty, express or implied, including the warranties of merchantability and fitness for a particular purpose, or assumes any legal liability or responsibility for the accuracy, completeness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. 


Author: James Fesmire <james.fesmire@ksc.nasa.gov> / NASA
Curator: David Adcock <david.adcock@ksc.nasa.gov> / NASA
Last Revised: April 28, 1997

A service of NASA / Kennedy Space Center Engineering Development Directorate, Mechanical GSE Division, Roger Hall, Chief (roger.hall-1@ksc.nasa.gov)