<?xml version="1.0" encoding="UTF-8"?>
<Spase xmlns="http://www.spase-group.org/data/schema">
    <Version>2.2.2</Version>
    <NumericalData>
        <ResourceID>spase://VWO/NumericalData/Cassini/RPWS/LRFULL_PT32S</ResourceID>
        <ResourceHeader>
            <ResourceName>Cassini RPWS Low Rate Full Resolution</ResourceName>
            <AlternateName>Cassini Orbiter Radio and Plasma Wave Science</AlternateName>
            <AlternateName>RPWS_RPWS_LOW_RATE_FULL</AlternateName>
            <ReleaseDate>2012-11-07T12:00:00.000Z</ReleaseDate>
            <Description>The Cassini Radio and Plasma Wave Science (RPWS) Low Rate Full Resolution Calibrated (RPWS_LOW_RATE_FULL) is a data set including all spectral density measurements acquired by the RPWS in units of electric or magnetic field spectral density.  This
      data set includes calibrated values for each frequency channel for
      each sensor for all times during the mission including the two
      Venus flybys, the Earth flyby, the Jupiter flyby, interplanetary
      cruise, and the entire Saturn tour.  Data for this data set are
      acquired from the RPWS Low Frequency Receiver (LFR), Medium
      Frequency Receiver (MFR), Medium Frequency Digital Receiver (MFDR)
      (which can be used to replace MFR band 2 data) and High Frequency
      Receiver (HFR).  Data are presented in a set of tables organized
      so as to have fixed-length records for ease in data handling.
      This data set is intended to be the most comprehensive and
      complete data set included in the Cassini RPWS archive.  A browse
      data set is included with these data which provides for a
      graphical search of the data using a series of thumbnail and
      full-sized spectrograms which lead the user to the particular data
      file(s) of interest.  This data set should be among the first used
      by a user of any of the RPWS archive as it will lead one to
      information required to search for more detailed or highly
      specialized products.

</Description>
            <Acknowledgement>When using this data please acknowledge the PI Donald A. Gurnett and Co-I William S. Kurth, NASA, the PDS and the VWO.</Acknowledgement>
            <Contact>
                <PersonID>spase://SMWG/Person/Donald.A.Gurnett</PersonID>
                <Role>PrincipalInvestigator</Role>
            </Contact>
            <Contact>
                <PersonID>spase://SMWG/Person/William.S.Kurth</PersonID>
                <Role>CoInvestigator</Role>
            </Contact>
            <Contact>
                <PersonID>spase://SMWG/Person/Raymond.J.Walker</PersonID>
                <Role>MetadataContact</Role>
            </Contact>
            <InformationURL>
                <Name>PDS/PPI</Name>
                <URL>http://ppi.pds.nasa.gov/</URL>
                <Description>NASA's Planetary Plasma Interactions (PPI) Node of the Planetary Data System (PDS)</Description>
            </InformationURL>
            <InformationURL>
                <Name>Cassini RPWS Volume CORPWS_0172</Name>
                <URL>http://ppi.pds.nasa.gov/archive1/CORPWS_0172/AAREADME.HTM</URL>
                <Description>The Cassini RPWS Volume 172 (typical) readme file with descriptions of the data, the organization of the data within the volume and associated software</Description>
            </InformationURL>
        </ResourceHeader>
        <AccessInformation>
            <RepositoryID>spase://SMWG/Repository/PDS/PPI</RepositoryID>
            <Availability>Online</Availability>
            <AccessRights>Open</AccessRights>
            <AccessURL>
                <Name>CO RPWS</Name>
                <URL>http://ppi.pds.nasa.gov/search/?k=CORPWS</URL>
                <Description>CASSINI ORBITER RADIO AND PLASMA WAVE SCIENCE</Description>
            </AccessURL>
            <Format>Text</Format>
            <Encoding>ASCII</Encoding>
            <Acknowledgement>Please acknowledge the P.I. and NASA's Planetary Plasma Interactions (PPI) Node of the Planetary Data System (PDS)</Acknowledgement>
        </AccessInformation>
        <ProviderResourceName>CO-V/E/J/S/SS-RPWS-3-RDR-LRFULL-V1.0</ProviderResourceName>
        <ProviderVersion>VERSION 1</ProviderVersion>
        <InstrumentID>spase://SMWG/Instrument/Cassini/RPWS</InstrumentID>
        <MeasurementType>Waves.Active</MeasurementType>
        <MeasurementType>Waves.Passive</MeasurementType>
        <MeasurementType>Spectrum</MeasurementType>
        <TemporalDescription>
            <TimeSpan>
                <StartDate>1997-10-25T00:00:00.000Z</StartDate>
                <RelativeStopDate>P300D</RelativeStopDate>
                <Note>The Cadence value is dependent on the operational mode. This value ranges from 64 seconds per cycle during cruise phase to as low as 8 seconds. In Saturn orbit, 32 seconds is the slowest cycle typically used.</Note>
            </TimeSpan>
		    <Cadence>PT32S</Cadence>
        </TemporalDescription>
        <SpectralRange>RadioFrequency</SpectralRange>
        <ObservedRegion>Venus</ObservedRegion>
        <ObservedRegion>Earth</ObservedRegion>
        <ObservedRegion>Jupiter</ObservedRegion>
        <ObservedRegion>Saturn</ObservedRegion>
        <ObservedRegion>Heliosphere</ObservedRegion>
        <Keyword>CASSINI ORBITER</Keyword>
        <Keyword>Venus</Keyword>
        <Keyword>Earth</Keyword>
        <Keyword>Jupiter</Keyword>
        <Keyword>Saturn</Keyword>
        <Keyword>Solar system</Keyword>
        <Keyword>Titan</Keyword>
        <Keyword>Enceladus</Keyword>
        <Keyword>Mimas</Keyword>
        <Keyword>Dione</Keyword>
        <Keyword>Tethys</Keyword>
        <Keyword>Phoebe</Keyword>
        <Keyword>Iapetus</Keyword>
        <Keyword>Hyperion</Keyword>
        <Keyword>Rhea</Keyword>
        <Keyword>CASSINI-HUYGENS</Keyword>
        <Parameter>
            <Name>FILE_ID</Name>
            <ParameterKey>FILE_ID</ParameterKey>
            <Description>'CORPWS01' for the file id.</Description>
            <Support>
                <SupportQuantity>Other</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>RECORD_LENGTH</Name>
            <ParameterKey>RECORD_LENGTH</ParameterKey>
            <Description>The length of each record in bytes.</Description>
            <Support>
                <SupportQuantity>Other</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>RECORDS</Name>
            <ParameterKey>RECORDS</ParameterKey>
            <Description>The total number of records.</Description>
            <Support>
                <SupportQuantity>Other</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>RECEIVER_TYPE</Name>
            <ParameterKey>RECEIVER_TYPE</ParameterKey>
            <Description>Logical RPWS Instrument ID Number.</Description>
            <Support>
                <SupportQuantity>Other</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>MINI_PACKET_HEADER</Name>
            <ParameterKey>MINI_PACKET_HEADER</ParameterKey>
            <Description>The mini-packet header which is representative     
                           for the data contained in the file.</Description>
            <Support>
                <SupportQuantity>Other</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>SCET</Name>
            <ParameterKey>SCET</ParameterKey>
            <Description>The standard JPL spacecraft event time description:
                           yyyy-doyThh:mm, seconds and milliseconds are       
                           assumed zero.  This is half of the SCLK/SCET       
                           pair produce by the SPICE kernel for the beginning 
                           of each day.</Description>
            <Support>
                <SupportQuantity>Temporal</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>SCLK</Name>
            <ParameterKey>SCLK</ParameterKey>
            <Description>The standard JPL spacecraft clock time description:
                           ssssssssss.fff.  This is half of the SCLK/SCET     
                           pair produce by the SPICE kernel for the beginning 
                           of each day.</Description>
            <Support>
                <SupportQuantity>Temporal</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>SCLK_SECOND</Name>
            <ParameterKey>SCLK_SECOND</ParameterKey>
            <Description>Spacecraft clock counter increments each
    second, beginning at approximately 1958-01-01T00:00:00Z.</Description>
            <Support>
                <SupportQuantity>Temporal</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>SCLK_PARTITION</Name>
            <ParameterKey>SCLK_PARTITION</ParameterKey>
            <Description>Spacecraft clock partition.
    A value of ZERO or ONE indicates the first partition
    (i.e. the spacecraft clock has not been reset).</Description>
            <Support>
                <SupportQuantity>Temporal</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>SCLK_FINE</Name>
            <ParameterKey>SCLK_FINE</ParameterKey>
            <Description>Spacecraft clock modulo 256 counter
    increments 256 times per second.  Since the RTI increments from
    0 through 7 in this same interval, SCLK_FINE / 32 yields the
    RTI count.
    For RPWS, SCLK_FINE is maintained within the instrument to an
    accuracy of one RTI period.  Time tags should occur only with
    the following values for SCLK_FINE : 0, 32, 64, 96, 128, 160,
    192, and 224</Description>
            <Support>
                <SupportQuantity>Temporal</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>SCET_DAY</Name>
            <ParameterKey>SCET_DAY</ParameterKey>
            <Description>Spacecraft event time days since
    1958-01-01T00:00:00Z</Description>
            <Support>
                <SupportQuantity>Temporal</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>SCET_MILLISECOND</Name>
            <ParameterKey>SCET_MILLISECOND</ParameterKey>
            <Description>Spacecraft event time millisecond
    of day allowing for up to two leap seconds.</Description>
            <Support>
                <SupportQuantity>Temporal</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>TIME</Name>
            <ParameterKey>TIME</ParameterKey>
            <Description>Time offset of individual samples            
                                  in corresponding columns relative           
                                  to time tag of each row.</Description>
            <Units>s</Units>
            <Structure>
                <Size>48</Size>
                <Description>Array of values</Description>
            </Structure>
            <Support>
                <SupportQuantity>Temporal</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>SCLK_SECOND</Name>
            <ParameterKey>SCLK_SECOND</ParameterKey>
            <Description>Spacecraft clock counter increments each
    second, beginning at approximately 1958-01-01T00:00:00Z.</Description>
            <Support>
                <SupportQuantity>Temporal</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>SCLK_PARTITION</Name>
            <ParameterKey>SCLK_PARTITION</ParameterKey>
            <Description>Spacecraft clock partition.
    A value of ZERO or ONE indicates the first partition
    (i.e. the spacecraft clock has not been reset).</Description>
            <Support>
                <SupportQuantity>Temporal</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>SCLK_FINE</Name>
            <ParameterKey>SCLK_FINE</ParameterKey>
            <Description>Spacecraft clock modulo 256 counter
    increments 256 times per second.  Since the RTI increments from
    0 through 7 in this same interval, SCLK_FINE / 32 yields the
    RTI count.
    For RPWS, SCLK_FINE is maintained within the instrument to an
    accuracy of one RTI period.  Time tags should occur only with
    the following values for SCLK_FINE : 0, 32, 64, 96, 128, 160,
    192, and 224</Description>
            <Support>
                <SupportQuantity>Temporal</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>SCET_DAY</Name>
            <ParameterKey>SCET_DAY</ParameterKey>
            <Description>Spacecraft event time days since
    1958-01-01T00:00:00Z</Description>
            <Support>
                <SupportQuantity>Temporal</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>SCET_MILLISECOND</Name>
            <ParameterKey>SCET_MILLISECOND</ParameterKey>
            <Description>Spacecraft event time millisecond
    of day allowing for up to two leap seconds.</Description>
            <Support>
                <SupportQuantity>Temporal</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>FREQUENCY</Name>
            <ParameterKey>FREQUENCY</ParameterKey>
            <Description>Frequency of spectral densities in           
                                  corresponding columns.</Description>
            <Units>Hz</Units>
            <Structure>
                <Size>48</Size>
                <Description>Array of values</Description>
            </Structure>
            <Support>
                <SupportQuantity>Other</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>ENGINEERING_DATA</Name>
            <ParameterKey>ENGINEERING_DATA</ParameterKey>
            <Description>This field contains the sensor ID number and   
                               data quality status.  Bits will be added as    
                               sources of interferance, telemetry errors,     
                               etc. are identified.  Individual data values   
                               within a capture are marked by multiplying     
                               the original measurement by negative one.</Description>
            <Support>
                <SupportQuantity>Other</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>ELECTRIC_SPECTRAL_DENSITIES</Name>
            <ParameterKey>ELECTRIC_SPECTRAL_DENSITIES</ParameterKey>
            <Description>Calibrated spectral densities from the
                                 electric antennas.</Description>
            <Units>V**2/m**2/Hz</Units>
            <Structure>
                <Size>48</Size>
                <Description>Array of values</Description>
            </Structure>
            <Wave>
                <WaveType>Electromagnetic</WaveType>
                <WaveQuantity>ACElectricField</WaveQuantity>
                <FrequencyRange>
                    <SpectralRange>RadioFrequency</SpectralRange>
                    <Low>1</Low>
                    <High>16000000</High>
                    <Units>Hz</Units>
                </FrequencyRange>
            </Wave>
        </Parameter>
        <Parameter>
            <Name>MAGNETIC_SPECTRAL_DENSITIES</Name>
            <ParameterKey>MAGNETIC_SPECTRAL_DENSITIES</ParameterKey>
            <Description>Calibrated spectral densities from the magnetic sensors.</Description>
            <Units>nT**2/Hz</Units>
            <Structure>
                <Size>48</Size>
                <Description>Array of values</Description>
            </Structure>
            <Wave>
                <WaveType>Electromagnetic</WaveType>
                <WaveQuantity>ACMagneticField</WaveQuantity>
                <FrequencyRange>
                    <SpectralRange>RadioFrequency</SpectralRange>
                    <Low>1</Low>
                    <High>12000</High>
                    <Units>Hz</Units>
                </FrequencyRange>
            </Wave>
        </Parameter>
    </NumericalData>
</Spase>
