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Thermal Protection Systems for Aerospace Vehicles During Atmospheric EntryAtmospheric entry and need for thermal protection systems (TPS) is discussed. Ceramic insulations for use as passive TPS are described. Different modes of heat transfer in ceramic insulation are described, and a thermal model is presented. Figures of merit for insulation performance are described and various methods for improving insulation performance are presented.
Document ID
20205007860
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Kamran Daryabeigi (Langley Research Center Hampton, Virginia, United States)
Date Acquired
September 22, 2020
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: Graduate Student Seminar, New Mexico State University
Location: Virtual
Country: US
Start Date: September 25, 2020
Sponsors: New Mexico State University
Funding Number(s)
WBS: 321991.02.23.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
thermal protection system
ceramic insulation

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