NASA NTRS · 20170006155
Thermal Protection Supplement for Reducing Interface Thermal Mismatch
Abstract
A thermal protection system that reduces a mismatch of thermal expansion coefficients CTE between a first material layer (CTE1) and a second material layer (CTE2) at a first layer-second layer interface. A portion of aluminum borosilicate (abs) or another suitable additive (add), whose CTE value, CTE(add), satisfies (CTE(add)-CTE1)(CTE(add)-CTE2)<0, is distributed with variable additive density,.rho.(z;add), in the first material layer and/or in the second material layer, with.rho.(z;add) near the materials interface being relatively high (alternatively, relatively low) and.rho.(z;add) in a region spaced apart from the interface being relatively low (alternatively, relatively high).
Keep this discovery
Explore connections, maps & timelines
Stewart, David A., Leiser, Daniel B.. 2017-06-27. Thermal Protection Supplement for Reducing Interface Thermal Mismatch. https://ntrs.nasa.gov/citations/20170006155
Cite the original work for its findings. Save a collection to share your selection of sources.