A family of aerogel-matrix composite materials having thermal-stability and mechanical-integrity properties better than those of neat aerogels has been developed. Aerogels are known to be excellent thermal- and acoustic-insulation materials because of their molecular-scale porosity, but heretofore, the use of aerogels has been inhibited by two factors:
- Their brittleness makes processing and handling difficult.
- They shrink during production and shrink more when heated to high temperatures during use. The shrinkage and the consequent cracking make it difficult to use them to encapsulate objects in thermal-insulation materials.
A material in the present family consists of a silica aerogel matrix reinforced with silica fibers and silica powder. The density of this composite material is typically only about 10 percent greater than the density of the corresponding neat aerogel. The underlying concept of aerogel-matrix composites is not new; the novelty of the present family of materials lies in formulations and processes that result in superior properties, which include (1) much less shrinkage during a supercritical-drying process employed in producing a typical aerogel, (2) much less shrinkage during exposure to high temperatures, and (3) as a result of the reduction in shrinkage, much less or even no cracking.
Synthesis of a composite aerogel of this type is based on a sol-gel process. The first step is to make a silica sol by refluxing and distilling a mixture of silicon alkoxide (tetramethyl ortho silicate, tetraethyl ortho silicate), a suitable solvent (methanol, ethanol), water, and nitric acid. The resultant concentrated sol is then diluted with acetonitrile. The second step is to prepare a solution for casting the composite aerogel: Fumed silica (325-mesh powder having specific surface area of about 200 m2/g) and silica powder (particle sizes between 1 and 2 μm) are suspended in acetonitrile and then the silica sol, water, and ammonium hydroxide base are added to the acetonitrile/powder suspension. The amount of each component can be adjusted to suit a specific application. After thus preparing the aerogel-casting solution, a piece of silica fiber felt (destined to become the fiber reinforcement in the composite) is placed in a mold. Then the aerogel-casting solution is poured into the mold, where it permeates the silica fiber felt (see Figure 1). After the solution has gelled, the casting is transferred to an autoclave filled with acetonitrile, wherein the casting is subjected to supercritical drying at a temperature of 295 °C and pressure of 5.5 MPa.
Heretofore, neat silica aerogels had been observed to undergo linear shrinkages between 5 and 10 percent upon supercritical drying. In tests of a composite of the present type, the incorporation of the silica fiber felt has been found to reduce the shrinkage to a negligible level (see Figure 2). The silica fiber felt seems to strengthen the aerogel and to serve as rigid framework that prevents shrinkage. It has been conjectured that the silica fiber felt divides the volume of the casting into small subvolumes, thereby confining strain to relatively small unit spaces (between fibers) instead of allowing strain to act over relatively large (millimeter to centimeter) lengths.
In other tests, a neat aerogel exhibited linear shrinkage of about 6 percent after exposure to a temperature of 1,000 °C in a vacuum for four hours, and an even greater shrinkage (about 50 percent) after four hours at 1,000 °C in air. In contrast, a composite aerogel of the present type exhibited no apparent shrinkage after 1 week at 1,000 °C in a vacuum, and a linear shrinkage of only about 2 percent after a week at 1,000 °C in air.
This work was done by Jong-Ah Paik, Jeffrey Sakamoto, and Steven Jones of Caltech for NASA’s Jet Propulsion Laboratory.
In accordance with Public Law 96-517, the contractor has elected to retain title to this invention. Inquiries concerning rights for its commercial use should be addressed to:
Innovative Technology Assets Management
JPL
Mail Stop 202-233
4800 Oak Grove Drive
Pasadena, CA 91109-8099
(818) 354-2240
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Refer to NPO-44287, volume and number of this NASA Tech Briefs issue, and the page number.
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Improved Silica Aerogel Composite Materials
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Overview
The document titled "Improved Silica Aerogel Composite Materials" (NPO-44287) from NASA's Jet Propulsion Laboratory outlines advancements in the development of silica aerogel composites aimed at enhancing their mechanical properties and thermal stability. Aerogels are known for their exceptional thermal and acoustic insulation due to their unique molecular-scale porosity. However, their widespread use has been limited by brittleness, processing challenges, and shrinkage during production, which can lead to cracking.
To address these issues, the document presents a solution involving the incorporation of low-density silica fiber felt (approximately 10 mg/cc) into the aerogel matrix. This approach effectively creates a composite material that improves the mechanical integrity and thermal stability of the aerogel while only slightly increasing its overall density. The silica fiber felt acts as a structural reinforcement, allowing the aerogel to better absorb stress and mitigate shrinkage during the drying process.
The synthesis of the composite aerogel follows a two-step sol-gel process. Initially, a silica sol is created using tetramethylorthosilicate (TMOS), methanol, acetonitrile, and nitric acid. This sol is then combined with fumed silica and silica powder to form a casting solution. The silica fiber felt is placed in a mold, and the aerogel solution is permeated into this network. After gelation, the samples undergo supercritical drying, which is crucial for achieving the desired aerogel properties.
The results indicate that incorporating silica fiber felt significantly reduces shrinkage during the drying process, eliminating it altogether in some cases. While traditional silica aerogels can shrink by approximately 10% after supercritical drying, the fiber-reinforced aerogels show negligible shrinkage. This characteristic allows for the encapsulation of devices with complex geometries without the risk of cracking.
Additionally, the document highlights the thermal stability of the composite aerogels, which can withstand temperatures up to 1000 °C with minimal shrinkage compared to standard silica aerogels. This advancement opens up new possibilities for applications in aerospace and other fields where robust thermal insulation is required.
In summary, the document presents a significant innovation in aerogel technology, showcasing a composite material that combines enhanced mechanical properties and thermal stability, addressing key challenges in the use of aerogels in practical applications.

