Parker Solar Probe, PSP, Integrated Science Investigation of the Sun, ISOIS, Energetic Particle Instrument, EPI-Hi, Rates: The Epoch time tags indicate midpoint of integration. For information concerning use of the ISOIS data please refer to the Energetic Particle Data User Guide available from the PSP ISOIS Science Operations Center, SOC, web site hosted by the University of New Hampshire. The energetic particle pitch angle calculations are made possible via use of magnetic field data provided by the PSP FIELDS team.
The public data reflect current instrument calibration as determined by the IS☉IS science team. Calibration efforts are ongoing and the public data will be updated over the course of the mission based on improved understanding of instrument response to the near-Sun energetic particle environment. IS☉IS visualization tools are provided as a quicklook utility for the community to better access the IS☉IS data and are also under continual development. While we make every effort to ensure their accuracy, the IS☉IS team cannot guarantee that they are error-free. For questions regarding the use of IS☉IS data, please contact Colin Joyce (cjjoyce@princeton.edu).
Refer to the following web site concerning the Rules of use for the ISOIS energetic particle data: http://spp-isois.sr.unh.edu/ISOIS_Terms_of_Use.html.
The PSP ISOIS effort is funded as part of the NASA Parker Solar Probe mission under contract NNN06AA01C. Use of any PSP ISOIS data in publications or presentations should include the following text for acknowledgement and also cite the PSP ISOIS instrument suite publication:
Acknowledgement: Thanks to the Integrated Science Investigation of the Sun (IS☉IS) Science Team (PI: D.J. McComas, Princeton University).
Citation: McComas, D.J. et al (2016). Space Sci. Rev., doi:10.1007/s11214-014-0059-1
Version:2.3.1
Parker Solar Probe, PSP, Integrated Science Investigation of the Sun, ISOIS, Energetic Particle Instrument, EPI-Hi, Rates: The Epoch time tags indicate midpoint of integration. For information concerning use of the ISOIS data please refer to the Energetic Particle Data User Guide available from the PSP ISOIS Science Operations Center, SOC, web site hosted by the University of New Hampshire. The energetic particle pitch angle calculations are made possible via use of magnetic field data provided by the PSP FIELDS team.
The public data reflect current instrument calibration as determined by the IS☉IS science team. Calibration efforts are ongoing and the public data will be updated over the course of the mission based on improved understanding of instrument response to the near-Sun energetic particle environment. IS☉IS visualization tools are provided as a quicklook utility for the community to better access the IS☉IS data and are also under continual development. While we make every effort to ensure their accuracy, the IS☉IS team cannot guarantee that they are error-free. For questions regarding the use of IS☉IS data, please contact Colin Joyce (cjjoyce@princeton.edu).
Refer to the following web site concerning the Rules of use for the ISOIS energetic particle data: http://spp-isois.sr.unh.edu/ISOIS_Terms_of_Use.html.
The PSP ISOIS effort is funded as part of the NASA Parker Solar Probe mission under contract NNN06AA01C. Use of any PSP ISOIS data in publications or presentations should include the following text for acknowledgement and also cite the PSP ISOIS instrument suite publication:
Acknowledgement: Thanks to the Integrated Science Investigation of the Sun (IS☉IS) Science Team (PI: D.J. McComas, Princeton University).
Citation: McComas, D.J. et al (2016). Space Sci. Rev., doi:10.1007/s11214-014-0059-1
| Role | Person | |
|---|---|---|
| 1. | PrincipalInvestigator | spase://SMWG/Person/David.J.McComas |
| 2. | MetadataContact | spase://SMWG/Person/Robert.M.Candey |
| 3. | MetadataContact | spase://SMWG/Person/Lee.Frost.Bargatze |
Parker Solar Probe, PSP, ISOIS Instrument Suite Description: McComas, D.J. et al., Integrated Science Investigation of the Sun (ISIS): Design of the Energetic Particle Investigation, Space Sci. Rev., 204, 187–256 (2016)
Parker Solar Probe, PSP, ISOIS Instrument Suite, Rules of the Road, Spacecraft Operations Center, SOC, web site, Univ. of New Hampshire
Parker Solar Probe, PSP, ISOIS Instrument Suite, Energetic Particle Data - User Guide, Spacecraft Operations Center, SOC, web site, Univ. of New Hampshire
Parker Solar Probe, PSP, ISOIS Instrument Suite, Spacecraft Operations Center, SOC, web site, Univ. of New Hampshire. This is the official science data host site for the IS☉IS instrument suite and visualization toolkit.
Parker Solar Probe, PSP, FIELDS Instrument Suite, Spacecraft Operations Center, SOC, web site, UC Berkeley. The magnetic field data sed for pitch angle calculation of ISOIS energetic particle data is provided courtesy of the PSP FIELDS team.
Access to Data in CDF Format via ftp from SPDF
Access to Data in CDF Format via http from SPDF
Access to ASCII, CDF, and Plots via NASA/GSFC CDAWeb
Electron, e-, Differential Count Rate, LET1, Side A
Epoch Time Tags, Nanoseconds since J2000 at Midpoint of the Integration
LET, Electron, e-, Bin Characteristic Energy Value for the Differential Count Rate Parameters
Epoch Time Delta Plus/Minus, one half of the Integration Time in Nanoseconds
LET, Electron, e-, Bin Characteristic Energy Value, Delta Minus, bin geometric center minus bin bottom, for the Differential Count Rate Parameters
LET, Electron, e-, Bin Characteristic Energy Value, Delta Plus, bin top minus bin geometric center, for the Differential Count Rate Parameters
Proton, H, Differential Count Rate, LET1, Side B
LET, Proton, H, Bin Characteristic Energy Value for the Differential Count Rate Parameters
LET, Proton, H, Bin Characteristic Energy Value, Delta Minus, bin geometric center minus bin bottom, for the Differential Count Rate Parameters
LET, Proton, H, Bin Characteristic Energy Value, Delta Plus, bin top minus bin geometric center, for the Differential Count Rate Parameters
Spacecraft Position at the Timestamp, Heliocentric Radial Distance, Heliocentric Inertial, HCI, Coordinates, Spherical
Proton, H, Differential Count Rate, HET, Side B
HET, Proton, H, Bin Characteristic Energy Value for the Differential Count Rate Parameters
HET, Proton, H, Bin Characteristic Energy Value, Delta Minus, bin geometric center minus bin bottom, for the Differential Count Rate Parameters
HET, Proton, H, Bin Characteristic Energy Value, Delta Plus, bin top minus bin geometric center, for the Differential Count Rate Parameters
LET1, Side A, Flow Direction for each Direction Bin, unit vector, Heliocentric Inertial, HCI, Coordinates, Cartesian
LET1, Side B, Flow Direction for each Direction Bin, unit vector, Radial-Tangential-Normal, RTN, Coordinates, Cartesian
LET1, Side A, Pitch Angle for each Direction Bin
Electron, e-, Differential Count Rate, HET, Side A
HET, Electron, e-, Bin Characteristic Energy Value for the Differential Count Rate Parameters
HET, Electron, e-, Bin Characteristic Energy Value, Delta Minus, bin geometric center minus bin bottom, for the Differential Count Rate Parameters
HET, Electron, e-, Bin Characteristic Energy Value, Delta Plus, bin top minus bin geometric center, for the Differential Count Rate Parameters
LET2, Side C, Flow Direction for each Direction Bin, unit vector, Radial-Tangential-Normal, RTN, Coordinates, Cartesian
HET, Side A, Flow Direction for each Direction Bin, unit vector, Radial-Tangential-Normal, RTN, Coordinates, Cartesian
Proton, H, Differential Count Rate, HET, Side A
HET, Side B, Flow Direction for each Direction Bin, unit vector, Heliocentric Inertial, HCI, Coordinates, Cartesian
Proton, H, Differential Count Rate, LET2, Side C
HET, Side A, Pitch Angle for each Direction Bin
Electron, e-, Differential Count Rate, LET2, Side C
Spacecraft Position at the Timestamp, Latitude, Heliographic Carrington, HGI, Coordinates, Spherical
Proton, H, Differential Count Rate, LET1, Side A
LET1, Side B, Pitch Angle for each Direction Bin
HET, Side A, Flow Direction for each Direction Bin, unit vector, Heliocentric Inertial, HCI, Coordinates, Cartesian
Spacecraft Position at the Timestamp, Heliocentric Radial Distance, Heliographic Carrington, HGI, Coordinates, Spherical
Spacecraft Position at the Timestamp, Longitude, Heliographic Carrington, HGI, Coordinates, Spherical
LET1, Side B, Flow Direction for each Direction Bin, unit vector, Heliocentric Inertial, HCI, Coordinates, Cartesian
Spacecraft Position at the Timestamp, Latitude, Heliocentric Inertial, HCI, Coordinates, Spherical
LET2, Side C, Pitch Angle for each Direction Bin
Electron, e-, Differential Count Rate, LET1, Side B
LET1, Side A, Flow Direction for each Direction Bin, unit vector, Radial-Tangential-Normal, RTN, Coordinates, Cartesian
LET2, Side C, Flow Direction for each Direction Bin, unit vector, Heliocentric Inertial, HCI, Coordinates, Cartesian
HET, Side B, Flow Direction for each Direction Bin, unit vector, Radial-Tangential-Normal, RTN, Coordinates, Cartesian
HET, Side B, Pitch Angle for each Direction Bin
Spacecraft Position at the Timestamp, Longitude, Heliocentric Inertial, HCI, Coordinates, Spherical
Electron, e-, Differential Count Rate, HET, Side B