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
- Cryogenic applications in the transportation, storage,
and transfer of cryogens;
- Near-room temperature applications such as refrigerator
insulation
- Elevated temperature applications such as insulation
for high-temperature industrial processes and furnaces.
Advantages
- Utilizied in both cryogenic and elevated temperatures
- High-performance CFC-free insulation
- Flexible and easy-to-use configuration (ideal insulation
for objects with irregular shapes)
- Lightweight and durable
- Available in blanket or clamshell (molded) product forms.
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)