Data Description

This page summarizes information about the selected resource and its origin based on SPASE metadata.

Table of Contents

  1. Product
  2. Repository
  3. Instrument
  4. Observatory
  5. Persons

SPASE version 2.0.0

Numerical Data Product: SOHO CELIAS Proton Monitor 30 Second Solar Wind data

Resource ID
spase://VHO/NumericalData/SOHO/CELIAS/PT30S Get XML
Name
SOHO CELIAS Proton Monitor 30 Second Solar Wind data
Description

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.

Additional information
SOHO Celias Proton Monitor Home Page

Site hosting instrument information, some data and plots for SOHO Celias PM

Acknowledgement

Please acknowledge the University of Maryland Space Physics Group

Contact
Role Person
1. Principal investigator Dr. Fred M. Ipavich Get XML
Release date
2009-05-20 19:08:29
Repository
Name
VHO and VMO Data Repository at NASA/GSFC Get XML
Availability
Online
Access rights
Open
URL
http://vho.nasa.gov/mission/soho/celias_pm_30sec/

CELIAS Proton Monitor repository at VHO

Format
Text
Encoding
ASCII
Instrument
Charge, Element, and Isotope Analysis System (CELIAS) Get XML
Measurement type
Thermal plasma
Temporal description
Start date
1996-01-20 20:17:30
Relative stop date
5 minutes ago
Cadence
30 seconds
Observed regions
Heliosphere.NearEarth
Caveats

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.

Parameters

Parameter #1

Name
Year
Parameter key
Field 1
Description

Two digit year

Parameter type
Temporal

Parameter #2

Name
Month
Parameter key
Field 2
Description

String representation of month

Parameter type
Temporal

Parameter #3

Name
Day
Parameter key
Field 3
Description

Day of the Month

Parameter type
Temporal

Parameter #4

Name
Time
Parameter key
Field 4
Description

Colon seperated day of year, hour, minute and second (doy:HH:MM:SS)

Parameter type
Temporal

Parameter #5

Name
Proton Speed
Parameter key
Field 5
Description

Proton Speed

Units
km/s
Particle type
Proton
Quantity
Velocity
Qualifier
Magnitude

Parameter #6

Name
Proton Density
Parameter key
Field 6
Description

Proton number density

Caveats

Parameters are derived from a combination of fitting and moment techniques

Units
cm^-3
Particle type
Proton
Quantity
Number density
Qualifier
Fit
Moment

Parameter #7

Name
Proton Thermal Speed
Parameter key
Field 7
Description

Most probable proton thermal speed

Caveats

Parameters are derived from a combination of fitting and moment techniques

Units
km/s
Particle type
Proton
Quantity
Thermal speed
Qualifier
Scalar
Moment
Fit

Parameter #8

Name
Proton arrival direction
Parameter key
Field 8
Description

Proton arrival direction in degrees from north/south with positive meaning from the south

Units
degrees
Particle type
Proton
Quantity
Velocity
Qualifier
Elevation angle

Parameter #9

Name
GSE X
Parameter key
Field 9
Description

GSE X Component of SOHO position vector based on predicted orbit files ( 1 Re = 6378 km )

Units
Re
Conversion to SI units
6.378e6>m
Coordinate system
Cartesian GSE
Parameter type
Positional

Parameter #10

Name
GSE Y
Parameter key
Field 10
Description

GSE Y Component of SOHO position vector based on predicted orbit files ( 1 Re = 6378 km )

Units
Re
Conversion to SI units
6.378e6>m
Coordinate system
Cartesian GSE
Parameter type
Positional

Parameter #11

Name
GSE Z
Parameter key
Field 11
Description

GSE Z Component of SOHO position vector based on predicted orbit files ( 1 Re = 6378 km )

Units
Re
Conversion to SI units
6.378e6>m
Coordinate system
Cartesian GSE
Parameter type
Positional

Parameter #12

Name
Heliocentric Range
Parameter key
Field 12
Description

Heliocentric Range of SOHO in 10^6 km

Units
millions of km (10^6 km)
Conversion to SI units
1e9>m
Parameter type
Positional

Parameter #13

Name
Heliographic latitude
Parameter key
Field 13
Description

Heliographic latitude of SOHO

Units
degrees
Parameter type
Positional

Parameter #14

Name
Heliographic longitude
Parameter key
Field 14
Description

Heliographic longitude of SOHO

Units
degrees
Parameter type
Positional

Parameter #15

Name
Earth Carrington Rotation Number
Parameter key
Field 15
Description

Earth Carrington Rotation Number

Parameter type
Temporal

SPASE version 2.0.0

Instrument: Charge, Element, and Isotope Analysis System (CELIAS)

Instrument ID
spase://SMWG/Instrument/SOHO/CELIAS Get XML
Name
Charge, Element, and Isotope Analysis System (CELIAS)
Alternate name
CELIAS
Description

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).

Additional information
NSSDC's Master Catalog

Information about the Charge, Element, and Isotope Analysis System (CELIAS) experiment on the SOHO mission.

Contact
Role Person
1. Principal investigator Dr. Dieter K. Hovestadt Get XML
Release date
2009-05-20 21:10:10
Instrument type
Energetic Particle Instrument
Investigation name
Charge, Element, and Isotope Analysis System (CELIAS) on SOHO
Observatory
SOHO Get XML

SPASE version 2.0.0

Observatory: SOHO

Observatory ID
spase://SMWG/Observatory/SOHO Get XML
Name
SOHO
Alternate name
1995-065A
Solar and Heliospheric Observatory
Description

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.

Additional information
NSSDC's Master Catalog

Information about the SOHO mission

Contact
Role Person
1. Project scientist Dr. Arthur I. Poland Get XML
Release date
2009-05-20 20:00:12
Location
Region
Heliosphere.NearEarth

SPASE version 2.0.0

Person: Dr. Fred M. Ipavich

Name
Dr. Fred M. Ipavich
Organization
University of Maryland
Person ID
spase://SMWG/Person/Fred.M.Ipavich Get XML

SPASE version 2.0.0

Person: Jan Merka

Name
Jan Merka
Organization
NASA Goddard Space Flight Center
Address
Code 672, Greenbelt, MD 20771, USA
Email
jan.merka@nasa.gov
Phone
1-301-286-8751
Person ID
spase://SMWG/Person/Jan.Merka Get XML
Release date
2007-08-09 22:02:24

SPASE version 2.0.0

Person: Dr. Dieter K. Hovestadt

Name
Dr. Dieter K. Hovestadt
Organization
Max-Planck-Institut fur Extraterrestrische
Person ID
spase://SMWG/Person/Dieter.K.Hovestadt Get XML

SPASE version 2.0.0

Person: Dr. Arthur I. Poland

Name
Dr. Arthur I. Poland
Organization
GSFC-Code 682
Email
poland@pal.gsfc.nasa.gov
Phone
+1-301-286-7076
Person ID
spase://SMWG/Person/Arthur.I.Poland Get XML
Release date
1999-08-18 00:00:00

SPASE version 1.2.0

Repository: VHO and VMO Data Repository at NASA/GSFC

Repository ID
spase://SMWG/Repository/NASA/GSFC/VHO-VMO Get XML
Name
VHO and VMO Data Repository at NASA/GSFC
Description

Data repository co-located with the VHO and VMO at NASA Goddard Space Flight Center.

Additional information
NASA/GSFC VHO/VMO Data Repository

The top-level directory of VHO/VMO data repository. (vho.nasa.gov server)

NASA/GSFC VHO/VMO Data Repository

The top-level directory of VHO/VMO data repository. (vmo.nasa.gov server)

Contact
Role Person
1. General contact
Technical contact
Jan Merka Get XML
Release date
2008-08-26 21:16:21
Prior ID
spase://VMO/Repository/VHO-VMO