Raman Spectroscopy System for Mars Surface Studies PI Bruce McIntosh PowerPoint PPT Presentation

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Title: Raman Spectroscopy System for Mars Surface Studies PI Bruce McIntosh


1
Raman Spectroscopy System for Mars Surface
StudiesPI Bruce McIntosh
  • OBJECTIVES
  • Development of a Raman spectrometer
  • system suitable for Mars rover operation
  • Science Mineral composition determination
  • Technology Laser, Probe, Spectrograph, software
    and camera optimization for Mars rover system.
  • Integration and testing of portable demonstration
    unit in environment similar to Mars surface

Co-Investigators   Requirements and Instrument
Specs. M. Bonner Denton (U. Ariz.
Tucson) Robert Downs (U. Ariz. Tucson . . .
2
FY04 Milestones
  • Assembly of Smart Raman Demonstrator Unit (SRDU)
  • Specify and procure custom spectrograph and probe
  • Receive and integrate custom spectrograph
  • Receive and integrate custom Raman probe
  • Receive and integrate diode laser module
  • Receive and integrate CCD camera assembly
  • Design and construct hardware interface subsystem
  • Create and Integrate Operating Software Suite
  • Customize existing Raman interface for new
    spectrograph
  • Create autofocus and hardware I/O program
  • Customize existing FTIR search software for Raman
    application
  • Format UofA Gem and Mineral Library for search
    module
  • Create overall system user interface program

3
Technical Accomplishments
  • All components for the complete SRDU have been
    received, tested and integrated.
  • All subsystems met purchase or design
    specifications
  • All custom and modified software operates with
    the hardware
  • High quality Raman spectra of reference materials
    and minerals were obtained.
  • A set of comparison tests were run on the SRDU
    and a commercial system.
  • SRDU performed equally or significantly better on
    all tests including resolution, spectral
    coverage, frequency accuracy, band shape and
    signal to noise ratio.
  • All components of required software are complete
    or nearing completion.
  • Only UI, auto-focus and search remain to be
    completed

4
Integration of SRDU System
  • System components received integrated and tested
    as complete Raman analyzer.
  • Performance goals for all components were met
    resulting in very high overall spectroscopic
    performance
  • Spectrometer, camera and camera controller
    -gt
  • Probe and laser in test enclosure -gt

5
Testing of Performance with Reference Materials
  • Spectra of a set of Raman standard materials was
    performed on SRDU and commercial System
  • SRDU has higher resolution.
  • SRDU has better band shape.
  • SRDU and commercial system both agreed with
    reference frequency values.
  • SRDU required lower power and shorter exposures
    to fill A/D converter range.
  • Figure to right shows cyclohexane sample spectra
  • 114mw 3 seconds Commercial (Purple)
  • 29mw 1 second SRDU (Red)

6
Testing of Performance with Mineral Samples
  • 10 Mars surrogate mineral samples were measured
    with both systems
  • SNR Figure of merit ranges from 3 to 50 times
    better than commercial system.
  • Spectrum to right shows Olivine with both
    systems.
  • RedSRDU PurpleCommercial

7
Testing of Auto-focus subsystem
  • Auto-focus subsystem
  • Captures visible image of laser spot through
    range of focus positions.
  • Calculates optimum focus by spot size.
  • Captures visible image of sample and superimposes
    laser spot image.
  • Olivine sample image is shown to right.
  • Red spot near center is laser image.
  • Image allows correlation of Raman signal with
    geometry of heterogeneous samples.
  • Laser spot at focus is 100u.
  • Note that image is through fast F/1.2 lens so
    focus is only clear around laser spot.

8
Plans for Next Period
  • Complete all remaining software integration tasks
  • Optimize performance of auto-focus
  • Perform further performance tests
  • Complete configuration and specification for
    flight Raman spectrometer
  • Prepare SRDU system for testing on NASA
    earthbound rover
  • Perform field tests, evaluate results and prepare
    report

9
Financial Status Obligations Cost
10
Financial Summary
  • Prior to June 04 spending was significantly below
    plan.
  • This was due to the decision to obtain major
    subsystems (spectrograph and probe) outside
    rather than fabricating them in-house.
  • These major items have now been received and
    accounted for bringing the spending and plan back
    into line.

11
Action Items/Issues/Concerns
  • All issues from last years report have been
    resolved
  • Consult with JPL on completion requirements
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