Data Set Information
DATA_SET_NAME ULY JUP SCE DOPPLER HI-RES DATA
DATA_SET_ID ULY-J-SCE-3-RDR-DOPPLER-HIRES-V1.0
NSSDC_DATA_SET_ID
DATA_SET_TERSE_DESCRIPTION ULY JUP SCE DOPPLER HI-RES DATA
DATA_SET_DESCRIPTION
Data Set Overview
      =================
      The Ulysses spacecraft was occulted by the Io Plasma Torus
      (IPT) during its Jupiter encounter on 8 February 1992. The
      Ulysses dual-frequency radio subsystem used by the Ulysses
      Solar Corona Experiment (SCE) was utilized to measure the
      electron content (column density) of the IPT [BIRDETAL1992B].
      In the nominal mode for radio-sounding observations
      [BIRDETAL1992A], both downlinks (S-band: f_s = 2.3 GHz;
      X-band: f_x = 8.4 GHz) are phase coherent with the uplink
      (S-band: f_u = 2.1 GHz). The dual-frequency radio-sounding
      technique exploits the dispersive nature of ionized media on
      the propagation of the two downlinks. The tiny Doppler shift
      due to plasma moving in and out of the ray path is greater
      at S-band than at the higher frequency X-band.

      The SCE data are obtained from the Radio Science Support group
      at JPL. There are basically two types of data: Ranging and
      Doppler (Frequency), recorded as a function of UT Ground
      Received Time. The raw data are delivered in special binary
      files called ATDFs (Archival Tracking Data Files), containing
      Ranging and Doppler data from the standard DSN tracking
      receivers. There are high-time resolution Doppler data from
      special radio science receivers (so-called 'open loop' data)
      as well. These are in files called ODRs (Original Data
      Records).

      ATDFs are files of radiometric data produced by the Network
      Operations Control Center (NOCC) Navigation Subsystem (NAV).
      They are derived from Intermediate Data Records by NAV and
      contain all radiometric measurements received from the DSN
      station including signal levels (`AGC' = automatic gain
      control in dBm), antenna pointing angles, frequency (often
      referred to simply as 'Doppler'), range, and residuals.
      Doppler data are often used to infer spacecraft radial motion
      relative to the tracking antenna. Data values in ATDFs are
      reported at rates no higher than 10 per second. For the
      Ulysses Jupiter encounter the received frequencies at S-Band
      and X-band were recorded at a sample time of one per second.
      Each ATDF data record contains 117 parameters, stored in
      records of 288 bytes. The ATDF is described in section
      TRK-2-25 of the JPL Document 820-13 [DSN820-13].

      The ATDFs have been analyzed for the Jupiter encounter and a
      detailed report has been published [BIRDETAL1993]. Data files
      have been generated which contain the Ranging and Doppler data
      at various stages of processing. Stage #1 is generally just
      stripping the Ranging/Doppler data from the ATDFs. Stage #2 is
      to 'clean' the data files by weeding out obviously bad data.
      Stage #3 is to produce a 'final data set', a table of the
      measured data plus physically relevant quantities as function
      of time.

      For the Doppler data, getting to stage #3 involves
      manipulating the frequency data to extract the changes in
      electron column density. An additional complication is the
      compensation for the Earth's ionosphere to separate its
      contribution from that of the Io Plasma Torus. This requires
      obtaining ionospheric calibration data from the DSN for the
      days of the Jupiter encounter. Details of the calibration
      procedure can be found in section TRK-2-23 of JPL document
      820-13 [DSN820-13]. Because the processing to stage #3 can be
      done in a variety of ways, it is best to leave the frequency
      measurements in their stage #2 form for the archiving process.
      In contrast to the modest volume of ranging data, the much
      higher sample rate increases the Doppler data volume to
      Megabyte proportions.

      Data
      ====
      The following tables give an idea about the size and coverage
      of the data set:

      Ulysses SCE Doppler data at Jupiter (complete set):

      Stage#     start        stop      ascii size
               doy:hh:mm    doy:hh:mm      (MB)
        1       36:15:45     41:15:44       72
        2       36:20:30     40:19:18       21

      The size of the data set has been reduced by providing only
      the Doppler data from the tracking passes at DSS 43/42 on
      Jupiter encounter day, when the spacecraft was occulted by the
      Io Plasma Torus. In this case the table of data becomes:

      Ulysses SCE Doppler data at Jupiter (encounter day only):

      Stage#     start        stop      ascii size
               doy:hh:mm    doy:hh:mm      (MB)
        1       39:03:15     40:00:00       16
        2       39:11:00     39:20:45        2

      Here are a few lines of the ASCII file at stage #2:

      ULS IPT OCCULTATION: 8 FEB 1992 (DOY 39)
      DSS 42/43:   S/X-BAND COHERENT
      10.25000 21.41667 0.7528 -2.5346 5.6032 3.4620 -1.4765 -2.5889
      time (hrs)    S-band phase       S-3/11X   AGC
      10.99999992   1566823818.441      -0.075  -150.9
      11.00027784   1567875175.345      -0.071  -150.9
      11.00055552   1568926527.281      -0.067  -151.3
      11.00083344   1569977874.261      -0.043  -151.1
      11.00111112   1571029216.279      -0.054  -151.6
      11.00138880   1572080553.284      -0.090  -151.3
      11.00166672   1573131885.437       0.010  -151.6

      where:
      time (hours) = time in hours on 8 FEB 1992 (DOY 39)
      S-Band phase = running S-band Doppler count (cycles)
      S-3/11X      = differential frequency (Hz)
      AGC          = S-band received signal level (dBm)

      and the row of numbers preceding the table gives the necessary
      parameters for the ionospheric calibration according to
      TRK-2-23 [DSN820-13] during this pass:

      tstart   tstop    c_0    c_1     c_2    c_3    c_4     c_5
      10.25000 21.41667 0.7528 -2.5346 5.6032 3.4620 -1.4765 -2.5889
      with
      tstart      = start time for the interval of ionospheric
                    calibration
      tstop       = stop time for the interval of ionospheric
                    calibration
      c_i, i=0,5  = polynomial coefficients for ionospheric
                    calibration
DATA_SET_RELEASE_DATE 1998-05-01T00:00:00.000Z
START_TIME 1992-02-08T11:00:00.000Z
STOP_TIME 1992-02-08T08:45:02.000Z
MISSION_NAME ULYSSES
MISSION_START_DATE 1990-10-06T12:00:00.000Z
MISSION_STOP_DATE N/A (ongoing)
TARGET_NAME JUPITER
TARGET_TYPE PLANET
INSTRUMENT_HOST_ID ULY
INSTRUMENT_NAME SOLAR CORONA EXPERIMENT
INSTRUMENT_ID SCE
INSTRUMENT_TYPE RADIO SCIENCE
NODE_NAME Planetary Plasma Interactions
ARCHIVE_STATUS ARCHIVED
CONFIDENCE_LEVEL_NOTE
Confidence Level Overview
      =========================
      None provided. For more information regarding the confidence
      level of this data set please contact:
        MICHAEL K. BIRD
        Radioastronomisches Institut
        Universitat Bonn
        Auf dem Hugel 71
        53121 Bonn
        GERMANY
        Phone: 49-228-733651 or 49-228-733675  Fax: 49-228-733672
        Internet: mbird@astro.uni-bonn.de
CITATION_DESCRIPTION Bird, M. K., ULY JUP SCE DOPPLER HI-RES DATA, ULY-J-SCE-3-RDR-DOPPLER-HIRES-V1.0, NASA Planetary Data System, 1998
ABSTRACT_TEXT The Ulysses spacecraft was occulted by the Io Plasma Torus (IPT) during its Jupiter encounter on 8 February 1992. The Ulysses dual-frequency radio subsystem used by the Ulysses Solar Corona Experiment (SCE) was utilized to measure the electron content (column density) of the IPT. In the nominal mode for radio-sounding observations, both downlinks (S-band: f_s = 2.3 GHz X-band: f_x = 8.4 GHz) are phase coherent with the uplink (S-band: f_u = 2.1 GHz). The dual-frequency radio-sounding technique exploits the dispersive nature of ionized media on the propagation of the two downlinks. The tiny Doppler shift due to plasma moving in and out of the ray path is greater at S-band than at the higher frequency X-band.
PRODUCER_FULL_NAME MICHAEL K. BIRD
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