NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
High efficiency tantalum-based ceramic composite structuresTantalum-based ceramics are suitable for use in thermal protection systems. These composite structures have high efficiency surfaces (low catalytic efficiency and high emittance), thereby reducing heat flux to a spacecraft during planetary re-entry. These ceramics contain tantalum disilicide, molybdenum disilicide and borosilicate glass. The components are milled, along with a processing aid, then applied to a surface of a porous substrate, such as a fibrous silica or carbon substrate. Following application, the coating is then sintered on the substrate. The composite structure is substantially impervious to hot gas penetration and capable of surviving high heat fluxes at temperatures approaching 3000.degree. F. and above.
Document ID
20100042283
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Stewart, David A.
Leiser, Daniel B.
DiFiore, Robert R.
Katvala, Victor W.
Date Acquired
August 25, 2013
Publication Date
August 3, 2010
Subject Category
Composite Materials
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-10/758,611
Patent Number: US-Patent-7,767,305
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-7,767,305
Patent Application
US-Patent-Appl-SN-10/758,611
No Preview Available