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Measurement of material recession and shock standoff in plasma windtunnel using neural netsArcjets are plasma wind tunnels used to test the performance of heatshield materials for spacecraft atmospheric entry. These facilities present an extremely harsh flow environment with heat fluxes up to 10^9 W/m^2 for up to 30 minutes. The plasma is low-temperature (~1 eV) but high pressure (> 10 kPa) creating high-enthalpy supersonic flows similar to atmospheric entry conditions. Typically, material samples are measured before and after a test to characterize the total recession. However, this does not capture time-dependent effects such as material expansion and non-linear recession.

This work will present new analysis of arcjet test videos which measure both the time-dependent 2D recession of the material samples and the shock standoff distance. New results showing non-linear material erosion rates will be highlighted. The material and shock edges are extracted from the videos by training and applying a convolutional neural network. Due to the consistent camera settings, the machine learning model achieves high accuracy (~99%) on new data with only a small number of training frames (~80).

The new results will be discussed in the context of temperature dependent plasma-surface interaction.
 
Document ID
20205006997
Acquisition Source
Ames Research Center
Document Type
Poster
Authors
Magnus A Haw
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Alexandre Marie Quintart
(University of Illinois at Urbana Champaign Urbana, Illinois, United States)
Date Acquired
August 31, 2020
Subject Category
General
Meeting Information
Meeting: APS Division of Plasma Physics Annual Meeting 2020
Location: Virtual
Country: US
Start Date: November 9, 2020
End Date: November 13, 2020
Sponsors: American Physical Society
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management

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