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Flexible Ablators Char Depths LHMEL Test ResultsChar and pyrolysis zone depths give physical evidence of peak temperature reached in depth: The pyrolyzing material acts as a temperature indicator within its characteristic thermal decomposition range. A matrix of novel flexible ablators were laser tested in one component of material screening for NASA Entry, Descent and Landing research for future Mars missions. LHMEL tests were run both on virgin materials, and on previously charred materials for a dual pulse simulation of the heating due to aerocapture followed by atmospheric entry. The test models were machined to expose the cross-sections. Char measurements were made at three locations near the center of the exposed area. Data are presented showing the char depths developed in these flexible materials, grouped by reinforcing fiber and pyrolyzing material type.
Document ID
20120011110
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
White, Susan
(NASA Ames Research Center Moffett Field, CA, United States)
Qu, Vince
(San Jose State Univ. San Jose, CA, United States)
Fan, Wendy
(ERC International, Inc. San Diego, CA, United States)
Stackpoole, Mairead
(ERC International, Inc. San Diego, CA, United States)
Thornton, Jeremy
(ERC International, Inc. San Diego, CA, United States)
Date Acquired
August 26, 2013
Publication Date
January 23, 2012
Subject Category
Aeronautics (General)
Report/Patent Number
ARC-E-DAA-TN4665
Report Number: ARC-E-DAA-TN4665
Meeting Information
Meeting: 36th Annual Conference on Composites, Materials, and Structures
Location: Cocoa Beach, FL
Country: United States
Start Date: January 23, 2012
End Date: January 26, 2012
Sponsors: American Ceramic Society
Funding Number(s)
CONTRACT_GRANT: NNA10DE12C
Distribution Limits
Public
Copyright
Public Use Permitted.
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