Tech Briefs

Microsphere Insulation Panels

Thermal performance and lifetime exceed those of foam insulation.

Microsphere insulation panels (MIPs) have been developed as lightweight, long lasting replacements for the foam and vacuum-jacketed systems heretofore used for thermally insulating cryogenic vessels and transfer ducts. Whether preformed or applied in place, foam insulation deteriorates fairly rapidly: on cryogenic transfer lines, it has a life expectancy of about three years. Vacuum-jacketed insulation is expensive and heavy. For both foam and vacuum-jacketed insulation, intensive maintenance is necessary to keep performance at or near its original level. Relative to a polyurethane foam insulation panel, a comparable MIP offers greater thermal performance and longer service life at approximately the same initial cost.

The microsphere core material of a typical MIP consists of hollow glass bubbles, which have a combination of advantageous mechanical, chemical, and thermal- insulation properties heretofore available only separately in different materials. In particular, a core filling of glass microspheres has high crush strength and low density, is noncombustible, and performs well in soft vacuum. A typical MIP includes microspheres in an evacuated space between flexible vacuum-barrier layers made of a multilayer polyester based laminate [Mylar® 250SBL300 (or equivalent)]. Included in the laminate are several non-foil layers that serve as barriers to permeation by water vapor and other atmospheric gases. The polyester based laminate material has a projected life in excess of 20 years.

An MIP can be made in clamshell-like halves that can be fitted into a cryogenic vessel or transfer duct. In general, MIPs can be applied to transfer ducts along with jacketing materials conventionally used on foam insulation, and can be installed by use of essentially the same techniques used to install preformed foam insulation. On the basis of tests according to standards C518 and C177 of the American Society for Testing and Materials, the thermal performance of a flexible vacuum-barrier MIP is about two times better than that of a comparable polyurethane foam insulation panel.

This work was done by R. Mohling, M. Allen, and R. Baumgartner of Technology Applications, Inc. for Kennedy Space Center. For further information, contact Rolf Baumgartner at (303) 443-2262 x115 or This email address is being protected from spambots. You need JavaScript enabled to view it. .

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: Technology Applications, Inc. 5700 Flatiron Parkway, #5701A Boulder, CO 80301-5733 Refer to KSC-12675, volume and number of this NASA Tech Briefs issue, and the page number.