This page summarizes information about the selected resource and its origin based on SPASE metadata.
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The Proton Monitor is a solar wind Energy per Charge (E/Q) analyzer of a new design, consisting of a three-box deflection system followed by a wedge-shaped MicroChannel Plate (MCP) assembly. The data are derived from sets of 6 rates (one for each voltage step of the PM deflection system) obtained every 30 seconds. The voltage steps are spaced logarithmically (about 60% step size) from about 0.3 to 3 kV. At a given voltage step the energy per charge dynamic range is slightly more than a factor of 2. The overall geometry factor of the PM is about 1.0 x 10**-4 cm**2.
Site hosting instrument information, some data and plots for SOHO Celias PM
Please acknowledge the University of Maryland Space Physics Group
| Role | Person | |
|---|---|---|
| 1. | Principal investigator | Dr. Fred M. Ipavich |
CELIAS Proton Monitor repository at VHO
On rare occassions the spacecraft's roll angle is changed for brief periods, during which the derived flow direction will refer to a different plane. A list of such times is available at http://umtof.umd.edu/pm/roll.html. In addition, since SOHO is not a spinning spacecraft, the deflection system was designed to have a wide angular acceptance (+- 15 deg). For technical reasons this leads to an ambiguity between incident angle and incident energy/charge; this ambiguity was designed into the PM to match as closely as possible the behavior of the deflection system for the main MTOF sensor. It is not the energy/charge but rather the mass/charge that is needed for interpretation of the MTOF mass data.
Two digit year
String representation of month
Day of the Month
Colon seperated day of year, hour, minute and second (doy:HH:MM:SS)
Proton Speed
Proton number density
Parameters are derived from a combination of fitting and moment techniques
Most probable proton thermal speed
Parameters are derived from a combination of fitting and moment techniques
Proton arrival direction in degrees from north/south with positive meaning from the south
GSE X Component of SOHO position vector based on predicted orbit files ( 1 Re = 6378 km )
GSE Y Component of SOHO position vector based on predicted orbit files ( 1 Re = 6378 km )
GSE Z Component of SOHO position vector based on predicted orbit files ( 1 Re = 6378 km )
Heliocentric Range of SOHO in 10^6 km
Heliographic latitude of SOHO
Heliographic longitude of SOHO
Earth Carrington Rotation Number
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This experiment, CELIAS (Charge, Element, and Isotope Analysis System), is designed to study the composition of the solar wind and of solar and interplanetary accelerated energetic particles. It consists of three different particle sensors, each optimized to one of these aspects, plus a fourth sensor to monitor the absolute EUV flux from the sun. The sensors are: Charge Time Of Flight (CTOF), solar wind Mass TOF (MTOF), Suprathermal TOF (STOF), and Solar Extreme-ultraviolet Monitor (SEM). The CELIAS particle energy ranges are designed to complement those of the COSTEP and ERNE experiments also on SOHO. The TOF sensors employ electrostatic deflection systems combined with TOF measurements. The CTOF covers the energy per charge range 0.1--55 KeV/charge, and will determine the composition, charge state distribution, kinetic temperature and speed of the more abundant solar wind ions (e.g., He, C, N, O, Ne, Mg, Si, and Fe). The field of view is a cone of 50 degrees. MTOF is a high-resolution retarding potential mass analyzer with a quadrapole electric field configuration, for measuring the composition of the less abundant elements in the solar wind, and also the isotopic composition of the more abundant heavy ions. The ions within the passband of the electrostatic section pass through a thin carbon foil, where they are scattered and emerge either as neutrals or singly-ionized. Secondary electrons emitted from the foil will generate the start signal, while the ions will generate the stop signal. The STOF is an ion telescope with 0.1 sq cm sr geometric factor. It covers 20--3000 KeV/charge with the electrostatic deflection system, and uses a TOF analysis similar to that of MTOF, plus a final energy measurement in a solid state detector. The SEM consists of a 5000 lines/mm gold transmission grating in front of a set of three absolutely calibrated silicon light diodes, which are covered with an aluminum filter (total thickness 150 nm). The diodes are placed at the zero- and first-order diffraction image of the sun to isolate the 30.4 nm He II line. Due to the extended source of the sun (0.5 degrees) and the 2 mm x 10 mm entrance slit, the spectrometer bandwidth is +/- 4.0 nm. There is a digital processing unit that serves all sensors. It receives, compresses, stores, and formats data for input into the spacecraft telemetry. This information is from the paper ``The Charge, Element, and Isotope Analysis System CELIAS on SOHO,'' by D. Hovestadt (Proceedings of the First SOHO Workshop, ESA SP-348, pp. 39-42, November 1992).
Information about the Charge, Element, and Isotope Analysis System (CELIAS) experiment on the SOHO mission.
| Role | Person | |
|---|---|---|
| 1. | Principal investigator | Dr. Dieter K. Hovestadt |
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The primary scientific aims of the Solar and Heliospheric Observatory mission (SOHO) were to investigate: (1) the physical processes that form and heat the Sun's corona, maintain it and give rise to the expanding solar wind; and, (2) the interior structure of the Sun. Imaging and collection of spectroscopic plasma diagnostics of the solar chromosphere, transition region and corona, as well as in situ solar-wind measurements are used to study the corona and solar wind. Solar interior structure is investigated by helioseismological means and by the observation of variations in solar irradiance. SOHO was part of the International Solar-Terrestrial Physics Program (ISTP).
The SOHO spacecraft was three-axis stabilized and pointed towards the Sun with an accuracy of +/- 10 arcsec per 15 min. It consisted of a Payload Module to accommodate the instruments and a Service Module carrying the spacecraft subsystems and solar arrays. SOHO occupied a halo orbit at the Earth-Sun L1 Lagrangian point to obtain uninterrupted sunlight. The design life was two years, but on-board consumables were sufficient for an extra four years of operations.
Twelve instruments comprised the payload, producing a continuous stream of data at 40 kbs, except whenever the solar oscillations imager Michelson Doppler Imager (MDI) was operated in high-bit-rate mode, producing 160 kbs. The high-bit-rate mode was used during scheduled daily eight-hour periods or during dedicated campaigns. Magnetic tape stored data between telemetry contacts with the Experiment Operations Facility, located at NASA-GSFC. For more information, see B. Fleck, V. Domingo, and A. I. Poland, eds., Solar Physics, V. 162, 1995.
SOHO was a joint mission of the European Space Agency and NASA. It was launched aboard an Atlas IIAS rocket from Cape Canaveral Air Station, FL, on Dec. 2, 1995, and mission operations were directed from NASA's Goddard Space Flight Center, Greenbelt, MD.
In April 1998, SOHO successfully completed its nominal two-year mission to study the Sun's atmosphere, surface and interior. Major science highlights include the detection of rivers of plasma beneath the surface of the Sun; the discovery of a magnetic "carpet" on the solar surface that seems to account for a substantial part of the energy that is needed to cause the very high temperature of the corona, the Sun's outermost layer; the first detection of flare-induced solar quakes; the discovery of more than 50 sungrazing comets; the most detailed view to date of the solar atmosphere; and spectacular images and movies of coronal mass ejections, which were being used to improve the ability to forecast space weather.
Contact with SOHO was lost at 23:16 GMT on June 24, 1998 during maintenance operations. The spacecraft went into emergency sun reacquisition mode, which is activated when an anomaly occurs and the spacecraft loses its orientation toward the Sun. When this happened, the spacecraft automatically tried to point itself toward the Sun again by firing its attitude control thrusters under the guidance of an onboard Sun sensor. Efforts to re-establish contact with SOHO did not succeed and telemetry was lost, not to be reestablished for several weeks.
Attitude analysis led to the conclusion that SOHO went into a spin such that the solar panels were nearly edge-on towards the Sun, and thus did not generate any power. Because the spin axis is fixed in space, as the spacecraft progressed in its orbit the orientation of the panels with respect to the Sun gradually changed, resulting in increased solar illumination of the solar arrays as time progressed. On August 3, contact was re-established with SOHO following six weeks of silence. After a lengthy recovery process, on September 16 the spacecraft again locked onto the Sun, and experiment heaters were switched on. After recommissioning of various subsystems, and an orbit correction maneuver, SOHO was finally brought back to normal mode on 25 September at 19:52:58 GMT. Instrument switch-on started October 5, 1998, and by November 4 all instruments were back to normal.
Information about the SOHO mission
| Role | Person | |
|---|---|---|
| 1. | Project scientist | Dr. Arthur I. Poland |
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Data repository co-located with the VHO and VMO at NASA Goddard Space Flight Center.
The top-level directory of VHO/VMO data repository. (vho.nasa.gov server)
The top-level directory of VHO/VMO data repository. (vmo.nasa.gov server)
| Role | Person | |
|---|---|---|
| 1. | General contact Technical contact | Jan Merka |