Instrument Information
IDENTIFIER urn:nasa:pds:context:instrument:vega2.mischa::1.0
NAME FLUXGATE MAGNETOMETER
TYPE MAGNETOMETER
DESCRIPTION
Scientific Overview
  ===================
    The magnetometer (MISCHA) The prime objective of the magnetometer
    experiment is to determine the role of the magnetic field in the
    interaction between the solar wind and the comet and to identify
    the characteristic boundaries of the cometary environment (bow
    shock, contact surface, etc.).
 
  Instrument Overview
  ===================
    The sensors of the MISCHA magnetometer are mounted on a boom. A
    single-axis sensor and a triaxial sensor are mounted 1 and 2 m,
    respectively, from the edge of the solar panel. The advantage of
    this dual-sensor fluxgate system is the possibility to determine
    the spacecraft's stray magnetic field.
 
    Magnetometer characteristics
    ----------------------------
      Dynamic range                 +/- 100 nT
      Resolution                    0.05 nT (12 bit)
      Noise level                   0.01 nT Hz**-1/2
      Zero drift                    +/- nT/month
      Bandwidth                     10 Hz
      Time resolution               10 vector/s
      (high-speed telemetry)        1 spectrum/25 s
      Number of frequency points    128/spectrum
 
    Detectors
    ---------
      MASS:
        triaxial sensor ... 500 g
        one-axis sensor ... 200 g
        electronic box ... 2200 g
 
    Operational Consdierations
    --------------------------
      MODE TRASSA 1
        TRASSA 1 (memory mode)
        this is the cruise phase mode;
        1 vector/2.5 min and 1 averaged spectrum/80 min
 
      MODE TRASSA 2
        TRASSA 2 (memory mode)
        2 days until 2 hours before Halley encounter and during
        selected cruise phase intervals (e.g. Venus tail crossing and
        ICE Giacobini-Zinner encounter);
        1 vector/min and 1 averaged spectrum/5 min
 
      MODE HIGH SPEED
        HIGH SPEED (memory mode)
        10 vector/min and 1 averaged spectrum/30 sec
 
      MODE Direct Transmission
        DT-65 (direct transmission)
        2 hours before until 2 hours after Halley encounter 10
        vectors/sec and 1 spectrum/25 sec
MODEL IDENTIFIER
NAIF INSTRUMENT IDENTIFIER not applicable
SERIAL NUMBER not applicable
REFERENCES Reinhard, R and B. Battrick (eds), 'Space Missions to Halley's Comet', European Space Agency ESA SP-1066, ESA Pub Div, Moordwijk, Netherlands, 1986.