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Ceramic Matrix Composite (CMC) Thermal Protection Systems (TPS) and Hot Structures for Hypersonic Vehicles
Document ID
20260005971
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
David E Glass (Langley Research Center Hampton, United States)
Date Acquired
July 3, 2026
Subject Category
Composite Materials
Meeting Information
Meeting: Thermal Protection Systems for Space Applications American Ceramic Society Course
Location: Houston, TX
Country: US
Start Date: August 4, 2026
End Date: August 5, 2026
Sponsors: American Ceramic Society
Funding Number(s)
WBS: 895366.01.07.08 AERX22026D
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
Hot structure
Composite materials
Hypersonics

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