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Orion EM-2 TPS Radiometer & SpectrometerRadiometers and Spectrometers embedded as flight instrumentation in a spacecraft's thermal protection system (TPS) can generate data on shock layer radiation to a spacecraft's surface for high-speed trajectories such as lunar return. Robust and accurate flight measurements of shock layer radiation can validate models and inform TPS selection and sizing, to reduce risk and TPS launch mass. Contamination from soot deposition and ablation products in the boundary layer condensing on a cold sapphire radiometer window or blocking open ports interferes with measurements. This poster describes characterization of the optical properties and performance of relevant materials, components, and contaminated windows, as well as investigation of contamination control strategies for the optics.
Document ID
20190004904
Acquisition Source
Ames Research Center
Document Type
Poster
Authors
White, Susan
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
May 2, 2019
Publication Date
September 24, 2018
Subject Category
Spacecraft Instrumentation And Astrionics
Report/Patent Number
AIAA-2015-3111
AIAA-2018-3590
AIAA-2012-0215
ARC-E-DAA-TN61384
Meeting Information
Meeting: Game Changing Development Annual Review (GCD 2018)
Location: Cleveland, OH
Country: United States
Start Date: September 24, 2018
End Date: September 28, 2018
Sponsors: NASA Glenn Research Center
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Ablation
Shock Layer Radiation
Instrumentation
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