Scanning Habitable Environments with Raman and Luminescence for Organics and Chemicals

Scanning Habitable Environments with Raman and Luminescence for Organics and Chemicals (SHERLOC) is an ultraviolet Raman spectrometer that uses fine-scale imaging and an ultraviolet (UV) laser to determine fine-scale mineralogy, and detect organic compounds designed for the Perseverance rover as part of the Mars 2020 mission.[1][2] It is constructed at the Jet Propulsion Laboratory with major subsystems being delivered from Malin Space Science Systems and Los Alamos National Laboratory. The Principal Investigator is Luther Beegle, and the Deputy Principal Investigator is Rohit Bhartia.

SHERLOC will have a calibration target with possible Mars suit materials, and it will measure how they change over time in the Martian surface environment.[3]

Goals

According to a 2017 Universities Space Research Association (USRA) report:[2]

The goals of the SHERLOC investigation are to:

  • Assess the habitability potential of a sample and its aqueous history.
  • Assess the availability of key elements and energy source for life (C, H, N, O, P, S etc.)
  • Determine if there are potential biosignatures preserved in Martian rocks and outcrops.
  • Provide organic and mineral analysis for selective sample caching.

To do this SHERLOC does the following:

  • Detects and classifies organics and astrobiologically relevant minerals on the surface and near subsurface of Mars
  • Bulk organic sensitivity of 10-5 to 10-6 w/w over a 7 x 7 mm spot.
  • Fine scale organic sensitivity of 10-2 to 10-4 w/w spatially resolved at <100µm
  • Astrobiologically Relevant Mineral (ARM) detection and classification to <100µm resolution
— Beegle, L.W., et al., USRA (2017)[2]

Construction

There are three locations on the rover where SHERLOC components are located. The SHERLOC Turret Assembly (STA) is mounted at the end of the rover arm. The STA contains spectroscopy and imaging components. The SHERLOC Body Assembly (SBA) is located on the rover chassis and acts as the interface between the STA and the Mars 2020 rover. The SBA deals with command and data handling, along with power distribution. The SHERLOC Calibration Target (SCT) is located on the front of the rover chassis and hold spectral standards.

SHERLOC consists of both imaging and spectroscopic elements. It has two imaging components consisting of heritage hardware from the MSL MAHLI instrument. One is a built to print re-flight that can generate color images over multiple scales. The other acts as the mechanism that allows the instrument to get a contextual image of a sample and to autofocus the laser spot for the spectroscopic part of the SHERLOC investigation.

For Spectroscopy, it utilizes a NeCu laser to generate UV photons (248.6 nm) which can generate characteristic Raman and fluorescence photons from a scientifically interesting sample. The deep UV laser is co-boresighted to a context imager and integrated into an autofocusing/scanning optical system that allows correlation of spectral signatures to surface textures, morphology and visible features. The context imager has a spatial resolution of 30 µm and currently is designed to operate in the 400-500 nm wavelength range.[4]

SHERLOC
instrument – outside
instrument – inside
test image

See also

References
  1. Webster, Guy (31 July 2014). "SHERLOC to Micro-Map Mars Minerals and Carbon Rings". NASA. Retrieved 31 July 2014.
  2. Beegle, L.W.; et al. (2017). "The SHERLOC Investigation For MARS 2020 (SHERLOC: Scanning Habitable Environments with Raman and Luminescence for Organics and Chemicals, an Investigation for 2020)" (PDF). Universities Space Research Association. Retrieved 30 August 2017.
  3. "The next NASA rover could lead to safer space suits for astronauts exploring Mars". The Mercury News. 20 February 2018. Retrieved 24 February 2018.
  4. Beegle, L.; Bhartia, R.; White, M.; DeFlores, L.; Abbey, W.; Wu, Yen-Hung; Cameron, B.; Moore, J.; Fries, M. (1 March 2015). "SHERLOC: Scanning habitable environments with Raman & luminescence for organics & chemicals". 2015 IEEE Aerospace Conference: 1–11. doi:10.1109/AERO.2015.7119105. ISBN 978-1-4799-5379-0.
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