DS-1/Plasma Experiment for Planetary Exploration (PEPE) PEPE – is a particle spectrometer capable of resolving energy, angle and mass & charge composition.

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Presentation transcript:

DS-1/Plasma Experiment for Planetary Exploration (PEPE) PEPE – is a particle spectrometer capable of resolving energy, angle and mass & charge composition of plasma electrons (Elc) protons (Ions single) Ions (composition, M/Q, TOF) Data coverage: 2001/ Encounter with Comet Borrelly on day 266 Files provided: mission.cat, insthost.cat datainfo.txt, data_product_def pdf calib_info.txt, pepe_borelly_ds.cat, pepe_inst.cat

Issues of PEPE’s information files 1.Instrumental & calibration parameters are spread through the various catalog files. 2. There is a description on how to generated phase space density (i.e. distribution functions) from the counts and instrumental parameters but the energy factor in the equation should be interpreted as energy per charge. 3. There is no description on the physical (meaningful) quantities that could be determined, formulas or algorithms on how to estimate them. 4. In the calibration file there is an incorrect labeling of Table 2 as detector efficiencies. They are detector solid angles (str). 5. For composition determination, a model dependent approach is suggested for the analysis, but no example are presented.

Instrument Characteristics (PEPE) ElectronsProtons/Ions *Energy Range (120 log-space steps) 8 eV – 31.5 keV Energy Resolution (  E/E) *Elevation Angle Range(4/8 steps) -45° - 45° *Azimuthal Angle Range(4/8 steps) 0°-360° Angular Resolution256 5°×5°, 5°×22°, 5°×45° Mass Range-1 – 135 amu Mass Resolution (M/  M) - 4(MR), 20(HR) Integration Time (  in ms) ms, ms * Telemetry Modes: 50bps, 1kbps

Moments Phase-Space Density: Geometrical Factor (G): G i,j,k = A  j,k (  E/E i )  Efficiency :  (  =1) Data Products: Moments of the distribution function f:

Electron Moments (ELC) Electrons in the SW are subsonic & sub-Alfvenic (i.e. U e << v the ) Density: Unit vectors e i,j,k = -(cos  az cos  el, sin  el, sin  az cos  el ). Average Energy (Temperature) in the proper frame: Bulk Velocity:

Electron Issues for Data Validation Efficiency factor  for density validation, cross-calibration with other spacecraft electron data to determine  accurately. It may also be angular dependent. Spacecraft potential (  spc ) corrections (photoelectrons, secondary electrons, etc). Electron background (or “glint”) counts subtraction. Poor angular resolution for other vectorial moment quantities such as: bulk velocity, temperature anisotropy, heat-flux. The data files are perhaps easily understood if the counts are formatted in matrix form with dependence on elevation, energy and time for each azimuth.

Proton Moments (Ions single) Protons in the SW are supersonic & super-Alfvenic (i.e. U p >> v thp ) Density: Bulk Velocity: Average Energy (Temperature) in the proper frame:

Proton Issues for Data Validation Efficiency factor  for density validation: cross-calibration with other spacecraft proton data to determine  accurately. It may also be angular dependent. Proton background counts correction (subtraction). To estimate the proton average temperature, it is necessary to subtract out the energy density due to bulk motion, thus an estimate of the proton bulk velocity U p is required. A possible way to estimate the magnitude of the proton bulk speed is to plot from the M/Q data, the counts (or phase space density) for bin 0 versus energy to obtain the maximum peak. Good angular resolution for other vectorial moment quantities such as: bulk velocity, temperature anisotropy, etc. The data files are perhaps easily understood if the counts are formatted in matrix form with dependence on elevation, energy and time for each azimuth.

Ion Composition Issues for Data Validation Model dependent  p are the unknown parameters to be determined by a minimization (Chi-Squared) method. Where the average counts model C model is obtained as follows: For example: f model can be represented by a Maxwellian distribution Unknown parameters p  (m s /q s, n s, U s, w th )