Calibration of Raman Bandwidths on the Scanning Habitable Environments with Raman and Luminescence for Organics and Chemicals (SHERLOC) Deep Ultraviolet Raman and Fluorescence Instrument Aboard the Perseverance Rover

Author:

Jakubek Ryan S.1ORCID,Bhartia Rohit2,Uckert Kyle3ORCID,Asher Sanford A.4,Czaja Andrew D.5ORCID,Fries Marc D.6,Hand Kevin3,Haney Nikole C.1,Razzell Hollis Joseph7,Minitti Michelle8,Sharma Shiv K.9,Sharma Sunanda3,Siljeström Sandra10

Affiliation:

1. Jacobs, NASA Johnson Space Center, Houston, Texas, USA

2. Photon Systems Incorporated, Covina, California, USA

3. Jet Propulsion Laboratory, California Institution of Technology, Pasadena, California, USA

4. Department of Chemistry, University of Pittsburgh, Pittsburgh, Pennsylvania, USA

5. Department of Geology, University of Cincinnati, Cincinnati, Ohio, USA

6. NASA Johnson Space Center, Houston, Texas, USA

7. The Natural History Museum, London, UK

8. Framework, Silver Spring, Maryland, USA

9. Hawaii Institute of Geophysics and Planetology, University of Hawaii, Honolulu, Hawaii, USA

10. RISE Research Institutes of Sweden, Stockholm, Sweden

Abstract

In this work, we derive a simple method for calibrating Raman bandwidths for the Scanning Habitable Environments with Raman and Luminescence for Organics and Chemicals (SHERLOC) instrument onboard NASA's Perseverance rover. Raman bandwidths and shapes reported by an instrument contain contributions from both the intrinsic Raman band (IRB) and instrumental artifacts. To directly correlate bandwidth to sample properties and to compare bandwidths across instruments, the IRB width needs to be separated from instrumental effects. Here, we use the ubiquitous bandwidth calibration method of modeling the observed Raman bands as a convolution of a Lorentzian IRB and a Gaussian instrument slit function. Using calibration target data, we calculate that SHERLOC has a slit function width of 34.1 cm–1. With a measure of the instrument slit function, we can deconvolve the IRB from the observed band, providing the width of the Raman band unobscured by instrumental artifact. We present the correlation between observed Raman bandwidth and intrinsic Raman bandwidth in table form for the quick estimation of SHERLOC Raman intrinsic bandwidths. We discuss the limitations of using this model to calibrate Raman bandwidth and derive a quantitative method for calculating the errors associated with the calibration. We demonstrate the utility of this method of bandwidth calibration by examining the intrinsic bandwidths of SHERLOC sulfate spectra and by modeling the SHERLOC spectrum of olivine.

Funder

Swedish National Space Agency

Jet Propulsion Laboratory

NASA Mars 2020 Returned Sample Science Participating Scientist Program

Publisher

SAGE Publications

Subject

Spectroscopy,Instrumentation

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