A new and improved composite flexible blanket insulation
(CBFI) has been developed at NASA Ames that is useful as a thermal protection
system for specific heating environments which contain conductive convective,
and radiative heating components. The CFBI provides an improved lightweight
insulation which is extremely effective in terms of thermal protection of
structures subjected singly or repeatedly to high heat fluxes.
The blanket has high emissivity and resistance to a high heat flux and thermal insulation capability up to 1400 degrees C (2550 degress F). By combining fabrics and sewing threads having a resistance to high heat flux and high emissivity with high break strength and a low density, lightweight CFBI can be designed to have commercially viable thermal insulation capability from 500 degrees C (920 degrees F) to 1400 degrees C (2550 degrees F). It provides flexible, durable, lightweight, high-temperature resistant insulation suitable for repeated use.
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NASA Ames is currently seeking partnerships with industry to further develop Composite Flexible Blanket Insulation capabilities while continuing to lower the cost. Licensing options are also available for the manufacture and distribution of this material. Composite Flexible Blanket Insulation, developed by Demetrius A. Kourtides and David M. Lowe, was issued U.S. Patent # 5,277,959 on January 11, 1994, which is assigned to The United States of America as represented by the Administrator of the National Aeronautics and Space Administration, Washington, D.C.
Thermal Protection Branch
Mail Stop 234-1
NASA Ames Research Center
Moffett Field, CA 94035-1000
Phone: (415)-604-4784
http://ctoserver.arc.nasa.gov:80/TechOpps/blanket.html
Composite Flexible Blanket Insulation (CFBI), Fire Fighting Equipment, Heat Resistant Sewing Thread, High Temperature Insulation, Protective Ceramic Coating. (PCC)