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Exploration of the Viability of HEEET as a TPS for Saturn, Neptune, and Uranus EntriesExploration of ballistic coefficient and entry flight path angle to determine loom requirements for weaving a dual-layer thermal protection material such as HEEET (Heatshield for Extreme Entry Environment Technology).
Document ID
20180007227
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Prabhu, Dinesh K. (Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Date Acquired
October 30, 2018
Publication Date
September 11, 2018
Subject Category
Composite Materials
Fluid Mechanics And Thermodynamics
Report/Patent Number
ARC-E-DAA-TN60961
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
HEEET
Atmospheric entry
thermal protection system

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