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Assessment of Fencing on the Orion HeatshieldThis paper presents recent experimental results from arc-jet tests of the Orion heatshield that were conducted at NASA Ames Research Center. Test conditions that simulated a set of heating profiles in time representative of the Orion flight environments were used to observe their effect on Orion's block architecture in terms of differential recession or fencing. Surface recession of arc-jet models was characterized during and after testing to derive fencing profiles used for the baseline sizing of the heatshield. Arc-jet test data show that the block architecture produces varying degrees of fencing.
Document ID
20160007545
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Alunni, Antonella I.
(Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Gokcen, Tahir
(Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Date Acquired
June 15, 2016
Publication Date
June 13, 2016
Subject Category
Fluid Mechanics And Thermodynamics
Spacecraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN27895
Report Number: ARC-E-DAA-TN27895
Meeting Information
Meeting: AIAA Thermophysics Conference
Location: Washington, DC
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Ground tests
Ablative materials
Thermal protection
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