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Thermal Protection MaterialsThermal protection materials and systems (TPS) are required to protect a vehicle returning from space or entering an atmosphere. The selection of the material depends on the heat flux, heat load, pressure, and shear and other mechanical loads imposed on the material, which are in turn determined by the vehicle configuration and size, location on the vehicle, speed, a trajectory, and the atmosphere. In all cases the goal is to use a material that is both reliable and efficient for the application. Reliable materials are well understood and have sufficient test data under the appropriate conditions to provide confidence in their performance. Efficiency relates to the behavior of a material under the specific conditions that it encounters TPS that performs very well at high heat fluxes may not be efficient at lower heat fluxes. Mass of the TPS is a critical element of efficiency. This talk will review the major classes of TPS, reusable or insulating materials and ablators. Ultra high temperature ceramics for sharp leading edges will also be reviewed. The talk will focus on the properties and behavior of these materials.
Document ID
20120002684
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Johnson, Sylvia M.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 25, 2013
Publication Date
September 20, 2011
Subject Category
Nonmetallic Materials
Report/Patent Number
ARC-E-DAA-TN4165
Report Number: ARC-E-DAA-TN4165
Meeting Information
Meeting: HI TEMP 2011 Conference
Location: Boston, MA
Country: United States
Start Date: September 20, 2011
End Date: September 22, 2011
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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