Data Set Information
DATA_SET_NAME ULYSSES JUPITER SOLAR CORONA EXPER. RANGING DATA 10 MIN AVG
DATA_SET_ID ULY-J-SCE-4-SUMM-RANGING-10MIN-V1.0
NSSDC_DATA_SET_ID
DATA_SET_TERSE_DESCRIPTION ULYSSES JUPITER SOLAR CORONA EXPER. RANGING DATA 10 MIN AVG
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.

      Data
      ====
      The following table gives an idea about the size and coverage
      of the ranging data set:

      Ulysses SCE Ranging data at Jupiter:

      Stage#     start        stop      ASCII size   gzip size
               doy:hh:mm    doy:hh:mm      (kB)        (kB)
        1       36:15:54     41:14:44      116          17
        2       36:20:30     40:18:44       88          13
        3       36:21:44     40:18:44       22           4

      All stage #3 ranging data from the Ulysses Jupiter encounter
      have been provided to this archive in the ALLRANGE directory.
       No ranging data were taken during the Jupiter encounter pass
      at DSS 43 on February 8, 1992. Here are the first few lines
      of the ASCII table:

      set  no dss  doy:hh:mm:ss  difrng   econt
        1   1  61   36:21:44:24       6      22
        1   2  61   36:21:54:24      53     210
        1   3  61   36:22: 4:24      16      62
        1   4  61   36:22:14:25      38     150
        1   5  61   36:22:44:24      67     266
        1   6  61   36:23: 4:24      47     186
        1   7  61   36:23:14:24      27     106
        1   8  61   36:23:24:24      60     238
        1   9  61   36:23:34:24      56     222

      where:
      set      = running number for each DSN tracking pass during
                 Jupiter encounter
      no       = running number for range measurement within each
                 tracking pass
      dss      = DSN station number
      doy      = Day of year in 1992
      hh:mm:ss = hours, minutes seconds (UT, ground received)
      difrng   = differential range delay in `range units' [DSN810-5]
      econt    = electron content in `hexems' [BIRDETAL1992B]
DATA_SET_RELEASE_DATE 1998-05-01T00:00:00.000Z
START_TIME 1992-02-05T09:44:24.000Z
STOP_TIME 1992-02-09T06:44:26.000Z
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
      =========================
      difrng (RU) and econt (hexems) are given to the nearest
      respective unit. The estimated accuracy of a differential
      range measurement is of the order of 50 range units.

      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., ULYSSES JUPITER SOLAR CORONA EXPER. RANGING DATA 10 MIN AVG, ULY-J-SCE-4-SUMM-RANGING-10MIN-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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