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Modern Advances in Ablative TPSTopics covered include: Physics of Hypersonic Flow and TPS Considerations. Destinations, Missions and Requirements. State of the Art Thermal Protection Systems Capabilities. Modern Advances in Ablative TPS. Entry Systems Concepts. Flexible TPS for Hypersonic Inflatable Aerodynamic Decelerators. Conformal TPS for Rigid Aeroshell. 3-D Woven TPS for Extreme Entry Environment. Multi-functional Carbon Fabric for Mechanically Deployable.
Document ID
20140000871
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Venkatapathy, Ethiraj (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
February 25, 2014
Publication Date
June 15, 2013
Subject Category
Aeronautics (General)
Report/Patent Number
ARC-E-DAA-TN9915
Report Number: ARC-E-DAA-TN9915
Meeting Information
Meeting: International Planetary Probe Workshop
Location: San Jose, CA
Country: United States
Start Date: June 15, 2013
End Date: June 16, 2013
Sponsors: San Jose State Univ.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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