AndreaBozzo/ceres-open-data-index huggingface dataset:
ROSETTA-ORBITER 67P RSI 1/2/3 PRELANDING 0208 V1.0

This is a Rosetta Radio Science data set, collected during the PRELANDING phase 2014-01-21 to 2014-11-18. It is a Global Gravity measurement at the comet 67P and covers the time 2014-08-15T08:22:55.000 to 2014-08-15T13:27:59.000.

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Organization: National Aeronautics and Space Administration
Ulysses Heliosphere Instrument for Spectral, Composition, and Anisotropy at Low Energies (HISCALE) LEFS120 Count Rates, 5 min Averages

5min-averaged sectored count rates from LEMS120. The HISCALE instrument contains the Low-Energy Magnetic Spectrometers (LEMS), the Low-Energy Foil Spectrometers (LEFS) and the Composition Aperture (CA). There is a LEMS detector at 30 degrees from the spacecraft spin axis and a second at 120 degrees. LEFS is positioned at 60 degrees from the spacecraft spin axis with a second LEFS detector at 150 degrees. The CA detector is positioned at 60 degrees from the spacecraft spin axis. The parameter descriptions of this document reference the detectors by their acronyms and angle from the spacecraft spin axis, i.e. LEMS30, LEMS120, LEFS60, LEFS150, and CA60.

Tags: energeticparticles
Organization: National Aeronautics and Space Administration
TWINS 1 Lyman Alpha Detector (LAD) Geocorona

TWINS, Two Wide-angle Imaging Neutral-atom Spectrometers, is a Mission of Opportunity under NASA's Small Explorer, SMEX, Program. TWINS-1 and TWINS-2 are the Designations for NASA-Sponsored Instruments flying on Unspecified Non-NASA U.S. Government Spacecraft. The TWINS-1 Instrument High Voltages were turned on in April 2007 and the TWINS-2 High Voltages were turned in May 2008; the Exact Launch Dates are not available. The Data, including both Science Data and Spacecraft Ephemeris and Attitude Information, from the two NASA-Funded Science Instruments are publicly available to the Scientific Research Community. See https://earth.esa.int/web/eoportal/satellite-missions/t/twins/ TWINS is a Stereo Mission whose overall Scientific Objective is to establish the Global Connectivities and Causal Relationships between Processes in Different Regions of the Earth's Magnetosphere. To meet this Goal, TWINS-1 and TWINS-2 provide Stereoscopic Neutral Atom Imaging of the Magnetosphere from Two Widely Spaced, High-Altitude, High-Inclination Spacecraft. TWINS Instrumentation includes an Energetic Neutral Atom, ENA, Imager to capture Charge-Exchange-Produced Neutral Atoms over a Broad Energy Range, approximately from 1 keV ro 100 keV, and a Lyman-alpha Detector to measure the Density of the Neutral Hydrogen Geocorona needed for Extraction of Magnetospheric Ion Fluxes from Neutral Atom Data. The TWINS-1 and TWINS-2 Instruments are identical. Each Spacecraft carrying TWINS Instruments is in a Molniya Orbit, 63.4°, 7.2 Re Apogee, 1000 km Perigee and Period 12 hr. The TWINS Spacecraft are 3-Axis stabilized and with Nadir-Pointing. Each acquires Image Data with Time Resolution of 60 s. The Time required to change Actuator Direction between Scans, an Interval with no Data Collection, was 25 s from June 2008 to July 2009, and 12 s at all other Times. This gives an Effective Cadence of 72 or 85 s. The Nominal Design Lifetime for each Instrument is four Years. TWINS operates only during the Apogee Portion of each Orbit, when the Spacecraft is above the Radiation Belts. The TWINS Lyman-alpha Detector consists of two independent Sensors to measure Lyman-alpha Radiation being emitted by Neutral Hydrogen Atoms. The Sensors oriented at Angles of 40° with respect to the Actuator Spin Axis. Each Sensor has a Full Width, Half Maximum, FWHM, Field-of-View of 4°, defined by Collimation Hole Baffles, uses Lyman-alpha Interference Filters as Narrow Band Transmissions Filters, and applies a KBr or CsI Photodiode for Photon Detection. The Lyman-alpha Detector is located on the rotating Actuator Platform to provide Full 360° Azimuthal Angle Coverage Time resolution is 60 s.

Tags: imageintensity
Organization: National Aeronautics and Space Administration
Pioneer 11 Ephemeris, Heliocentric Trajectories, Heliographic, Heliographic Inertial, and Solar Ecliptic Coordinates, HelioWeb, Daily Data

Heliocentric trajectories for Pioneer 11 in Heliographic, HG, Heliographic Inertial, HGI, and Solar Ecliptic, SE, Coordinates The original trajectory data are taken from http://ssd.jpl.nasa.gov/horizons.cgi where users can find many more objects. In the case of orbit data for planets, the orbit data can be used as a proxy for spacecraft ephemeris that are in orbit about the planets. On a heliospheric scale, differences between the planet orbital tarjectory and that of the spacecraft are very small. For instance, the heliocentric longitudes differ by only 0.25° for a spacecraft stationed near the L1 Lagrange point at approximately 100 Earth radii upstream of the Earth. The production of the HG, HGI, and SE trajectory data requires a values for the "Equinox Epoch", which is defined as the epoch time when the direction from the Earth to the sun at the time of the vernal equinox when the sun seems to cross equatorial plane of the Earth from below. This direction is called the First Point of Aries, FPA and it is not a fixed direction but drifts by about 1.4° per century or 50.26" per year. In addition, there are tiny irregularities in FPA drift that are on the order of 1" per year or less. The Equinox Epoch can be determined by using a variety of methods for calculating the instantaneous FPA longitudinal direction and whether the tiny irregularities have been smoothed or averaged out. Four methods for determining the Equinox Epoch are in common usage: +---------------------------------------------------------------------+   Method Name   FPA Longitude Definition    ---------------------------------------------------------------------    B1950.0   the actual FPA at 22:09 UT on December 31, 1949     J2000.0   the smoothed FPA at 12:00 UT on January 1, 2000     True of Date   the actual FPA at 00:00 UT on the date of interest     Mean of Date   the smoothed FPA at 00:00 UT on the date of interest   +---------------------------------------------------------------------+ The heliocentric trajectory data included in this data product have been calculated by using the Equinox Epoch: defined via the "Mean of Date" method. More precise coordinates, and some planet-centered coordinates, are found in the "traj" subdirectories of spacecraft specific directories at https://spdf.gsfc.nasa.gov/pub/data/ and http://ssd.jpl.nasa.gov/horizons.cgi.

Tags: ephemeris
Organization: National Aeronautics and Space Administration
Ulysses Heliosphere Instrument for Spectral, Composition, and Anisotropy at Low Energies (HISCALE) LEFS150 MFSA, Spacecraft Frame, Sectored Z>1 Ion Fluxes, Daily Averages

Daily-averaged sectored Z>1 ion fluxes from the MF Spectrum Analyzer of the Ulysses/HISCALE LEFS150 instrument. All energies thresholds take into account the incident particle type, shielding, and inactive dead-layer of the solid state detector. All fluxes are background corrected and are in the spacecraft rest frame.

Tags: energeticparticles
Organization: National Aeronautics and Space Administration
GALILEO SSI/IDA RADIOMETRICALLY  CALIBRATED IMAGES V1.0

This data set includes Galileo Orbiter  SSI radiometrically calibrated images of the asteroid 243 Ida, created using ISIS software and assuming nadir pointing. This is an original  delivery of radiometrically calibrated files, not an update to  existing files. All images archived include the asteroid within the  image frame. Calibration was performed in 2013-2014.

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Organization: National Aeronautics and Space Administration
Ulysses Heliosphere Instrument for Spectral, Composition, and Anisotropy at Low Energies (HISCALE) LEFS150 MFSA, Spacecraft Frame, Sectored Proton Fluxes, Hourly Averages

Hourly-averaged sectored proton fluxes from the MF Spectrum Analyzer of the Ulysses/HISCALE LEFS150 instrument. All energies thresholds take into account the incident particle type, shielding, and inactive dead-layer of the solid state detector. All fluxes are background corrected and are in the spacecraft rest frame.

Tags: energeticparticles
Organization: National Aeronautics and Space Administration
ROSETTA-ORBITER 67P RSI 1/2/3 COMET ESCORT 1 0485 V1.0

This is a Rosetta Radio Science data set, collected during the COMET ESCORT 1 phase 2014-11-20 to 2015-03-10. It is a Global Gravity measurement at the comet 67P and covers the time 2014-12-12T03:24:15.000 to 2014-12-12T13:06:36.500.

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Organization: National Aeronautics and Space Administration
Ulysses Heliosphere Instrument for Spectral, Composition, and Anisotropy at Low Energies (HISCALE) LEFS60 MFSA, Solar Wind Frame, Sectored Electron Fluxes, Daily Averages

Daily-averaged sectored electron fluxes from the MF Spectrum Analyzer of the Ulysses/HISCALE LEFS60 instrument. All energies thresholds take into account the incident particle type, shielding, and inactive dead-layer of the solid state detector. All fluxes are background corrected and are in the solar wind rest frame.

Tags: energeticparticles
Organization: National Aeronautics and Space Administration
Ulysses Heliosphere Instrument for Spectral, Composition, and Anisotropy at Low Energies (HISCALE) LEFS60 MFSA, Solar Wind Frame, Sectored Electron Fluxes, 17 min Averages

17-min-averaged sectored electron fluxes from the MF Spectrum Analyzer of the Ulysses/HISCALE LEFS60 instrument. All energies thresholds take into account the incident particle type, shielding, and inactive dead-layer of the solid state detector. All fluxes are background corrected and are in the solar wind rest frame.

Tags: energeticparticles
Organization: National Aeronautics and Space Administration
Ulysses Heliosphere Instrument for Spectral, Composition, and Anisotropy at Low Energies (HISCALE) LEFS60 MFSA, Solar Wind Frame, Sectored Proton Fluxes, Hourly Averages

Hourly-averaged sectored proton fluxes from the MF Spectrum Analyzer of the Ulysses/HISCALE LEFS60 instrument. All energies thresholds take into account the incident particle type, shielding, and inactive dead-layer of the solid state detector. All fluxes are background corrected and are in the solar wind rest frame.

Tags: energeticparticles
Organization: National Aeronautics and Space Administration
VEGA2 DUST PARTICLE IMPACT DETECTOR DATA V1.0

The SP-2 experiment on Vega spacecraft was intended for studying the spatial and mass distributions of dust particles in the cometary coma over the mass range 1.e-16 to 1.e-6 g. Covering such a broad mass range was made possible by using sensors of two types, namely, impact plasma and acoustic.

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Organization: National Aeronautics and Space Administration
Ulysses Heliosphere Instrument for Spectral, Composition, and Anisotropy at Low Energies (HISCALE) LEFS60 MFSA, Solar Wind Frame, Sectored Z>1 Ion Fluxes, Daily Averages

Daily-averaged sectored Z>1 ion fluxes from the MF Spectrum Analyzer of the Ulysses/HISCALE LEFS60 instrument. All energies thresholds take into account the incident particle type, shielding, and inactive dead-layer of the solid state detector. All fluxes are background corrected and are in the solar wind rest frame.

Tags: energeticparticles
Organization: National Aeronautics and Space Administration
MARS EXPRESS ASPERA-3 RAW-CAL NTRL PARTICLE IMAGER EXT6 V1.0

This data set contains Mars Express ASPERA-3 Neutral         Particle Imager (NPI) data for the sixth mission extension         (January 1, 2017 - Dec. 31, 2018).  These data are provided         in units of count rate (counts/second).

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Organization: National Aeronautics and Space Administration
Ulysses Heliosphere Instrument for Spectral, Composition, and Anisotropy at Low Energies (HISCALE) LEFS60 MFSA, Solar Wind Frame, Sectored Z>1 Ion Fluxes, 17 min Averages

17-min-averaged sectored Z>1 ion fluxes from the MF Spectrum Analyzer of the Ulysses/HISCALE LEFS60 instrument. All energies thresholds take into account the incident particle type, shielding, and inactive dead-layer of the solid state detector. All fluxes are background corrected and are in the solar wind rest frame.

Tags: energeticparticles
Organization: National Aeronautics and Space Administration
Ulysses Heliosphere Instrument for Spectral, Composition, and Anisotropy at Low Energies (HISCALE) LEFS60 MFSA, Solar Wind Frame, Sectored Proton Fluxes, 17 min Averages

17-min-averaged sectored proton fluxes from the MF Spectrum Analyzer of the Ulysses/HISCALE LEFS60 instrument. All energies thresholds take into account the incident particle type, shielding, and inactive dead-layer of the solid state detector. All fluxes are background corrected and are in the solar wind rest frame.

Tags: energeticparticles
Organization: National Aeronautics and Space Administration
MARS EXPRESS ASPERA-3 FLUX DDR ION MASS ANALYZER EXT4 V1.0

This data set contains Mars Express ASPERA-3 Ion Mass         Analyzer (IMA) data for the fourth mission extension         (January 1, 2013 - January 1, 2015).         The data are provided in units of Differential Number Flux,         m-2 s-1 sr-1 eV-1

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Organization: National Aeronautics and Space Administration
ROSETTA-ORBITER 67P OSINAC 4 ESC1-MTP010 RDR-INFLDSTR V1.0

This CODMAC level 4 data set contains solar stray-light corrected, in-field stray-light corrected,  radiometric calibrated and geometric distortion corrected  (resampled) image data in W/m^2/sr/nm,  acquired by the OSIRIS Narrow Angle Camera on the Rosetta spacecraft  during the COMET ESCORT 1 mission phase, covering the period  from 2014-11-21T23:25:00.000 to 2014-12-19T23:24:59.000. The prime target is comet 67P/Churyumov-Gerasimenko 1 (1969 R1). This version V1.0 is the first version of this dataset: Lien corrected dataset after September 2019 PSA/PDS external peer review.

Tags: __
Organization: National Aeronautics and Space Administration
Ulysses Heliosphere Instrument for Spectral, Composition, and Anisotropy at Low Energies (HISCALE) LEFS60 MFSA, Spacecraft Frame, Sectored Electron Fluxes, 17 min Averages

17-min-averaged sectored electron fluxes from the MF Spectrum Analyzer of the Ulysses/HISCALE LEFS60 instrument. All energies thresholds take into account the incident particle type, shielding, and inactive dead-layer of the solid state detector. All fluxes are background corrected and are in the spacecraft rest frame.

Tags: energeticparticles
Organization: National Aeronautics and Space Administration
Ulysses Heliosphere Instrument for Spectral, Composition, and Anisotropy at Low Energies (HISCALE) LEFS150 Count Rates, 11.5 s Averages

12sec-averaged sectored count rates from LEFS150. The HISCALE instrument contains the Low-Energy Magnetic Spectrometers (LEMS), the Low-Energy Foil Spectrometers (LEFS) and the Composition Aperture (CA). There is a LEMS detector at 30 degrees from the spacecraft spin axis and a second at 120 degrees. LEFS is positioned at 60 degrees from the spacecraft spin axis with a second LEFS detector at 150 degrees. The CA detector is positioned at 60 degrees from the spacecraft spin axis. The parameter descriptions of this document reference the detectors by their acronyms and angle from the spacecraft spin axis, i.e. LEMS30, LEMS120, LEFS60, LEFS150, and CA60.

Tags: energeticparticles
Organization: National Aeronautics and Space Administration
GSSR V RTLS 5 12.6-12.9CM RADAR SCALED ECHO POWER/ALT V1.0

The Goldstone Solar System Radar observations of Venus from 1972 until 1988 are included in this data set. The system operated at 12.6 cm up until 1977 operated at 12.9 cm. The data consist of radar scaled backscatter cross sections in image format and, in most cases, associated altimetry observations. The data were acquired over 52 separate observing runs. In total the observations cover the region between approximately 260 degrees (leftmost) east longitude to 30 degrees (rightmost) east longitude, within approximately 20 degrees of the equator. Backscatter data were acquired with opposite sense circular polarization with incidence angles typically less than 10 degrees. Associated altimetric data were acquired using a two or three station interferometric system. Data are presented in Mercator projection with degrees/pixel in longitude dependent on the individual data file.

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Organization: National Aeronautics and Space Administration
Ulysses Heliosphere Instrument for Spectral, Composition, and Anisotropy at Low Energies (HISCALE) LEFS60 MFSA, Spacecraft Frame, Sectored Z>1 Ion Fluxes, 17 min Averages

17-min-averaged sectored Z>1 ion fluxes from the MF Spectrum Analyzer of the Ulysses/HISCALE LEFS60 instrument. All energies thresholds take into account the incident particle type, shielding, and inactive dead-layer of the solid state detector. All fluxes are background corrected and are in the spacecraft rest frame.

Tags: energeticparticles
Organization: National Aeronautics and Space Administration
DAWN VESTA GRAVITY SCIENCE DERIVED SCIENCE DATA V2.0

This data set contains archival results from gravity investigationsconducted during the Dawn mission while the spacecraft was in orbitaround the asteroid Vesta. Radio measurements were made using theDawn spacecraft and Earth-based stations of the NASA Deep SpaceNetwork (DSN). The data set includes a spherical harmonic modelof Vesta's gravity field generated by the Jet Propulsion Laboratoryand radial gravity acceleration map; these results werederived from raw radio tracking data.

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Organization: National Aeronautics and Space Administration
Ulysses Heliosphere Instrument for Spectral, Composition, and Anisotropy at Low Energies (HISCALE) LEFS60 MFSA, Spacecraft Frame, Sectored Z>1 Ion Fluxes, Daily Averages

Daily-averaged sectored Z>1 ion fluxes from the MF Spectrum Analyzer of the Ulysses/HISCALE LEFS60 instrument. All energies thresholds take into account the incident particle type, shielding, and inactive dead-layer of the solid state detector. All fluxes are background corrected and are in the spacecraft rest frame.

Tags: energeticparticles
Organization: National Aeronautics and Space Administration
DEEP IMPACT 9P/TEMPEL ENCOUNTER - RAW HRIV NAV IMAGES V1.0

This data set contains raw 9P/Tempel 1 and calibration images acquired by the Deep Impact High Resolution Instrument Visible CCD during the encounter phase of the mission. These observations were used for optical and autonomous navigation (NAV) of the flyby spacecraft as well as for scientific investigations. These data were collected from 3 June to 4 July 2005.

Tags: __
Organization: National Aeronautics and Space Administration
Ulysses Heliosphere Instrument for Spectral, Composition, and Anisotropy at Low Energies (HISCALE) LEFS150 Count Rates, 5 min Averages

5min-averaged sectored count rates from LEFS150. The HISCALE instrument contains the Low-Energy Magnetic Spectrometers (LEMS), the Low-Energy Foil Spectrometers (LEFS) and the Composition Aperture (CA). There is a LEMS detector at 30 degrees from the spacecraft spin axis and a second at 120 degrees. LEFS is positioned at 60 degrees from the spacecraft spin axis with a second LEFS detector at 150 degrees. The CA detector is positioned at 60 degrees from the spacecraft spin axis. The parameter descriptions of this document reference the detectors by their acronyms and angle from the spacecraft spin axis, i.e. LEMS30, LEMS120, LEFS60, LEFS150, and CA60.

Tags: energeticparticles
Organization: National Aeronautics and Space Administration
Ulysses Heliosphere Instrument for Spectral, Composition, and Anisotropy at Low Energies (HISCALE) LEFS60 MFSA, Spacecraft Frame, Sectored Proton Fluxes, 17 min Averages

17-min-averaged sectored proton fluxes from the MF Spectrum Analyzer of the Ulysses/HISCALE LEFS60 instrument. All energies thresholds take into account the incident particle type, shielding, and inactive dead-layer of the solid state detector. All fluxes are background corrected and are in the spacecraft rest frame.

Tags: energeticparticles
Organization: National Aeronautics and Space Administration
Ulysses Heliosphere Instrument for Spectral, Composition, and Anisotropy at Low Energies (HISCALE) LEFS60 MFSA, Spacecraft Frame, Sectored Proton Fluxes, Daily Averages

Daily-averaged sectored proton fluxes from the MF Spectrum Analyzer of the Ulysses/HISCALE LEFS60 instrument. All energies thresholds take into account the incident particle type, shielding, and inactive dead-layer of the solid state detector. All fluxes are background corrected and are in the spacecraft rest frame.

Tags: energeticparticles
Organization: National Aeronautics and Space Administration
ROSETTA-ORBITER LUTETIA MIDAS 3 AST2 LUTE V3.0

The Micro-Imaging Dust Analysis System (MIDAS) is an instrument on theROSETTA Orbiter that will provide 3D images and statistical parametersof pristine cometary particles, collected in the vicinity of comet67P/Churyumov-Gerasimenko. This data set includes all data from theLUTETIA FLY-BY mission phase.This release supersedes version 1.0. Version 2.0 was never generatedfor pre-comet phases.

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Organization: National Aeronautics and Space Administration
Ulysses Heliosphere Instrument for Spectral, Composition, and Anisotropy at Low Energies (HISCALE) LEMS120 MFSA, Solar Wind Frame, Sectored Z>1 Ion Fluxes, Daily Averages

Daily-averaged sectored Z>1 ion fluxes from the MF Spectrum Analyzer of the Ulysses/HISCALE LEMS120 instrument. All energies thresholds take into account the incident particle type, shielding, and inactive dead-layer of the solid state detector. All fluxes are background corrected and are in the solar wind rest frame.

Tags: energeticparticles
Organization: National Aeronautics and Space Administration
CCD IMAGES OF 19P/BORRELLY, 1987-2002

This data set presents images and photometry of comet 19P/Borrelly 1 obtained by Karen Meech over 20 nights during the period 1987-08-21 to 2002-02-03. These data were not of sufficient quality to be reviewed or formally ingested.

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Organization: National Aeronautics and Space Administration
Ulysses Heliosphere Instrument for Spectral, Composition, and Anisotropy at Low Energies (HISCALE) LEFS60 Count Rates, Daily Averages

Daily-averaged sectored count rates from LEFS60. The HISCALE instrument contains the Low-Energy Magnetic Spectrometers (LEMS), the Low-Energy Foil Spectrometers (LEFS) and the Composition Aperture (CA). There is a LEMS detector at 30 degrees from the spacecraft spin axis and a second at 120 degrees. LEFS is positioned at 60 degrees from the spacecraft spin axis with a second LEFS detector at 150 degrees. The CA detector is positioned at 60 degrees from the spacecraft spin axis. The parameter descriptions of this document reference the detectors by their acronyms and angle from the spacecraft spin axis, i.e. LEMS30, LEMS120, LEFS60, LEFS150, and CA60.

Tags: energeticparticles
Organization: National Aeronautics and Space Administration
MARS EXPRESS SUN MRS 1/2/3 EXTENDED MISSION 5 3777 V1.0

This is a Mars Express Radio Science data set, collected during the extended mission phase 2015-01-01 to 2016-12-31. It is a Solar Conjunction measurement and covers the time 2015-06-23T11:48:01 to 2015-06-23T17:39:00.

Tags: __
Organization: National Aeronautics and Space Administration