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Effects of Laser Wavelength on Ablator TestingWavelength-dependent or spectral radiation effects are potentially significant for thermal protection materials. NASA atmospheric entry simulations include trajectories with significant levels of shock layer radiation which is concentrated in narrow spectral lines. Tests using two different high powered lasers, the 10.6 micron LHMEL I CO2 laser and the near-infrared 1.07 micron fiber laser, on low density ablative thermal protection materials offer a unique opportunity to evaluate spectral effects. Test results indicated that the laser wavelength can impact the thermal response of an ablative material, in terms of bond-line temperatures, penetration times, mass losses, and char layer thicknesses.
Document ID
20140011553
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
White, Susan M.
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
September 10, 2014
Publication Date
January 27, 2014
Subject Category
Composite Materials
Aeronautics (General)
Report/Patent Number
ARC-E-DAA-TN12788
Report Number: ARC-E-DAA-TN12788
Meeting Information
Meeting: Annual Conference on Composites, Materials, and Structures
Location: Cape Canaveral, Florida
Country: United States
Start Date: January 27, 2014
End Date: January 31, 2014
Sponsors: United States Advanced Ceramics Association
Funding Number(s)
WBS: WBS 470883.04.01.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
thermal protection
radiation
fiber composites
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