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Background Information Spacecraft charging
Spacecraft charging: data sets

The charging data given here consist of two databases which are available at ESA. They contain ion and electron fluxes as measured by two satellites, Gorizont 91/2 (ADIPE) and CRRES (LEPA). The data that has been used is the data that was reported by Rodgers [1994] to contain charging events for the Gorizont satellite and by Rodgers and Johnstone [1994] for the CRRES data. The description below was taken from these references.

Gorizont 91/2: ADIPE

The Gorizont satellites are a series of telecommunication satellites in geostationary orbit. These satellites carried, in addition to their main payload, instruments to monitor the space environment. These satellites are geostationary and have one axis permanently directed at the Earth. Gorizont 91-2 had longitude 80°E and started operating on November 25th, 1991. Data from 25/11/1991 untill 29/09/1993 has been processed for charging analysis.

The ADIPE instrument

ADIPE is the spectrometric and dosimetric instrument group of instruments on the Gorizont satellites produced by the Scientific Production Association of Applied Mechanics (NPO-PM) in Krasnoyarsk. The instrument package operates automatically and consists of a faraday cup, a cylindrical electrostatic analyser, solid state detectors, gas discharge counters, Cherenkov counters and gas proportional counters. The main data rate is 128s. The information presented here comes from the ion and electon electrostatic analysers.

Summary table of charging events

The table summarises the charging characteristics of the days which contain charging events. Graphs of each event are available by selecting the date in the first column. The information in the table was taken from Rodgers [1994].

In the table, the times given and the potential reached are based on visual interpretation of the data plots and hence are subjective. Multiple charging events on the same day are listed separately where the spacecraft appears to return to its normal state in-between. The duration of the data in each file is listed in decimal hours but when two events are in the same file a dash replaces the duration for the second event. The eclipse flag is shown where the spacecraft was in eclipse for part of the charging event. In practice, there were often non-eclipse charging events on these days also, but the maximum potential usually occurred during the eclipse phase. The electron signature flag is set when electron charging was seen. In general, a distinct rise and fall in energy of the electron peak was required before being identified as being due to charging. Many intense bursts of electrons were seen at other times and it is not yet clear whether these are natural or the result of some differential potential. The electron potential is the maximum differential charging as deduced from the electron charging signature. When two simultaneous peaks were seen, maximum values for both are quoted. The electron potential was always lower than the ion charging potential.

Graphs

The particle measurements were used to produce a set of graphical representations of the charging events. Each of the graphs is available as a GIF file; links to PostScript versions are provided as well.

The first graph is a panel plot showing five variables as a function of time. The two top panels are spectograms which show the temporal evolution of the plasma data (ions above and electrons below). The flux levels are represented by logarithmic colour scales. The fluxes shown are the fluxes along the spacecraft Z-axis. The next two panels show the parameters of a double Maxwellian fit to the electron spectra, and the last plot shows B/B0 and McIlwain's L parameter as a function of time. For the last plot, the UNILIB Library (developed by BIRA-IASB) was used. Links to tables with the fit parameters and magnetic coordinates are provided.

The next three graphs represent electron spectra taken at three different times. The first spectrum corresponds to conditions before charging occurs, the second one is taken at the beginning of the charging event and the third one near the maximum charging level. The spectograms also contain a SCATHA worst case plot and a double Maxwellian approximation of the spectrum. The parameters of the fitted function are given with each graph.

CRRES: LEPA

CRRES (Combined Release and Radiation Effects Satellite) was launched on 25 July 1990, into a geostationary transfer orbit inclined at 18° to the Earth's equatorial plane, with apogee at 6.3 Earth radii. Apogee was at 0830 MLT shortly after launch, processing effectively westwards about the Earth as the Earth orbited the Sun, until apogee had reached 0330 MLT by the end of the mission in late 1991.

LEPA

The Low Energy Plasma Analyser (LEPA) measures electrons and ions in the energy range 10 eV to 30 keV. The instrument was intended to provide fully three dimensional distributions within this energy range, while retaining sufficient angular resolution to examine the populations entering and leaving the loss cones. LEPA consists of two 260° electrostatic analysers, with a single arc-segment microchannel plate on each. The information presented in this section and the charging event plots were made available by Mullard Space Science Laboratory (MSSL).

Summary table of charging events

The CRRES orbits on which charging events occurre, are listed with the date and the time when the charging events can be seen. For most orbits, a plot of the whole orbit and a higher resolution plot of the charging event are available. The McIlwain L values were calculated with IGRF85 internal geomagnetic field model and the Olson-Pfitzer 1977 external field model. The listed L range corresponds to the L value at the start and end of the event. The maximum potential was always negative and is listed in volts. When charging potentials were so high that the ion peak linked up with the ambient hot ions, it is not possible to distinguish the burst ions as a separate population and such occasions are identified by '?' in the table.

Two charging events on orbit 279 are listed separately. Some doubt still remains in the identification of the events on orbits 809 and 856 as charging events. The signature of a brief charging event appears to be present on these orbits but the background count rate was too high for the ion peaks to be clearly identified in both the perpendicular and parallel look directions.

The two most intense charging events were during eclipses on orbits 425 and 431. On these days eclipse occurred from 11:22:00 to 12:07:00 and 22:52:00 to 23:07:00, respectively. The duration of the charging events matched closely the duration of the eclipse. All the other events occurred in sunlight.

Graphs

The charging events are represented as spectograms which show the temporal evolution of the plasma data (electrons above and ions below). The flux levels are represented by logarithmic colour scales. The fluxes shown are the fluxes along the three directions (perpendicular, Equatorward and Earthward parallel to B).

References

Rodgers, D. J., Evaluation of Russian Spacecraft Charging Data, Chapter 6 in Final Report On Rider 2, Estec Contract No. 7989/88/NL/PB(SC), 1994.

Rodgers, D. J. and A. D. Johnstone, Analysis of CRRES Charging Events, Chapter 3 in Final Report on Rider 2, Estec Contract No. 7989/88/NL/PB(SC), 1994.


Last update: Mon, 12 Mar 2018