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    <Identification_Area>
        <logical_identifier>urn:nasa:pds:context:instrument:otes.orex</logical_identifier>
        <version_id>1.0</version_id>
        <title>The OSIRIS-REx Thermal Emission Spectrometer (OTES) aboard the OSIRIS-REx spacecraft</title>
        <information_model_version>1.7.0.0</information_model_version>
        <product_class>Product_Context</product_class>
        <Modification_History>
            <Modification_Detail>
                <modification_date>2018-03-14</modification_date>
                <version_id>1.0</version_id>
                <description>Initial version</description>
            </Modification_Detail>
        </Modification_History>
    </Identification_Area>
    <Reference_List>
        <Internal_Reference>
            <lid_reference>urn:nasa:pds:context:instrument_host:spacecraft.orex</lid_reference>
            <reference_type>instrument_to_instrument_host</reference_type>
        </Internal_Reference>
        <External_Reference>
            <reference_text>
                P.R. Christensen, V.E. Hamilton, G.L. Mehall, D. Pelham, W.O'Donnell, S. Anwar, H. Bowles, S. Chase, J. Fahlgren, Z. Farkas, T. Fisher, O. James, I. Kubik, I. Lazbin, M.Miner, M. Rassas. L. Schulze, K. Shamordola, T. Tourville, G. West, R. Woodward, and D. Lauretta. The OSIRIS-REx Thermal Emission Spectrometer (OTES) Instrument, Space Science Reviews, submitted, 2018.
            </reference_text>
            <description>The OTES instrument paper.</description>
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    </Reference_List>
    <Instrument>
        <name>OTES</name>
        <type>Spectrometer</type>
        <description>The OSIRIS-REx Thermal Emission Spectrometer (OTES) is a small infrared (4-50 µm) point spectrometer that
         acquires an interferogram every 2 seconds. Interferograms are processed on the ground and converted to infrared spectra. 
         OTES uses space and internal calibration target views for calibration. OTES will map Bennu and the sample site from a 
         distance of 7 to 0.5 km with 55 to 4 m resolution using spacecraft and asteroid motion. 
        </description>
    </Instrument>
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