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: THEMIS-A: Solid State Telescope (SST): Energy flux spectrogram, electron/ion ground-calculated fluxes (30 keV - 300 keV).

Resource ID
spase://VMO/NumericalData/THEMIS/A/SST/PT3S Get XML
Name
THEMIS-A: Solid State Telescope (SST): Energy flux spectrogram, electron/ion ground-calculated fluxes (30 keV - 300 keV).
Alternate name
THEMIS-A SST
Description

THEMIS-A: The Solid State Telescope (SST) measures the incoming intensity (flux per solid angle) of superthermal electrons and ions. The spacecraft is fitted with two units (heads), each SST unit has two pairs of opposing ion and electron sensors. Each single sensor covers an angle of 36 degrees. The units are oriented such that one pair is always centered in the rotation plane, the other oriented at a maximum angle of 54 degrees off the plane. Each pair of units are oriented opposite each other allowing both ion and electron sensors to sweep out a maximum of 92% of the sky (45x45 degree required Elevation by Azimuth FOV, 108x22 raw) . The ion and electron sensors primarily measure particles between 30-300 keV and 30-100 keV respectively with a maximum capability of 20-6000 keV and 25-1000 keV. Full distribution data is measured over 128 angles and 16 energy bins, reduced distribution uses 6 angles and 16 energy bins, and burst mode data has 64 angles in 16 energy bins. Matched and paired electron broom magnets produce quadrapole fields reducing magnetic contamination. A mechanical attenuator is used to increase the instruments dynamical range avoiding oversaturation near the plasma sheet edge.

Acknowledgement

NASA Contract NAS5-02099

Contact
Role Person
1. Principal investigator Dr. Vassilis Angelopoulos Get XML
2. CoInvestigator Mr. Davin Larson Get XML
3. CoInvestigator Prof. Robert P. Lin Get XML
Release date
2009-05-20 23:06:02
Repository
Name
CDAWeb Data Repository FTP Interface Get XML
Availability
Online
Access rights
Open
URL
CDAWeb FTP Access

NASA/GSFC CDAWeb ftp access to the data.

ASCII, CDF, and plots from CDAWeb

Access to ASCII, CDF, and plots via NASA/GSFC CDAWeb

Format
CDF
Encoding
None
Processing level
Calibrated
Provider processing level
Level 2
Provider version
xxxx
Instrument
THEMIS-A: Solid State Telescope (SST): Energy flux spectrogram, electron/ion ground-calculated fluxes (30 keV - 300 keV). Get XML
Measurement type
Energetic particles
Ion composition
Spectrum
Temporal description
Start date
2007-03-14 01:00:00
Relative stop date
7 days ago
Cadence
3 seconds
Caveats

Calibration for the SST is not complete. Currently there are no corrections for the dead layer. Other data products will be added later as calibration continues. Total list of expected data types can be found on the THEMIS website.

Parameters

Parameter #1

Name
SST Ion energy spectrogram
Parameter key
tha_psif_en_eflux
Description

SST Ion energy spectrogram in DSL (Despun Spacecraft) coordinates. Spectrogram data is averaged over solid angle.

Caveats

DSL coordinates: The Z-axis points towards the spacecraft spin axis and the Y-axis is obtained from the cross product of Z and the Spacecraft-Sun direction as viewed from the probe; X completes a right handed system.

Units
eV/(cm^2*s*sr*eV)
Conversion to SI units
1e4>1/(m^2*s*sr)
Coordinate system
Cartesian SR2
Structure
Size
16
Elements
Index Name Valid min Valid max Fill value
1 tha_psif_en_eflux_1 0.0 1.0E10 NaN
2 tha_psif_en_eflux_2 0.0 1.0E10 NaN
3 tha_psif_en_eflux_3 0.0 1.0E10 NaN
4 tha_psif_en_eflux_4 0.0 1.0E10 NaN
5 tha_psif_en_eflux_5 0.0 1.0E10 NaN
6 tha_psif_en_eflux_6 0.0 1.0E10 NaN
7 tha_psif_en_eflux_7 0.0 1.0E10 NaN
8 tha_psif_en_eflux_8 0.0 1.0E10 NaN
9 tha_psif_en_eflux_9 0.0 1.0E10 NaN
10 tha_psif_en_eflux_10 0.0 1.0E10 NaN
11 tha_psif_en_eflux_11 0.0 1.0E10 NaN
12 tha_psif_en_eflux_12 0.0 1.0E10 NaN
13 tha_psif_en_eflux_13 0.0 1.0E10 NaN
14 tha_psif_en_eflux_14 0.0 1.0E10 NaN
15 tha_psif_en_eflux_15 0.0 1.0E10 NaN
16 tha_psif_en_eflux_16 0.0 1.0E10 NaN
Particle type
Ion
Quantity
Number flux
Qualifier
Differential
Anisotropy

Parameter #2

Name
SST Ion energy spectrogram Y-axis (energy).
Parameter key
tha_psif_en_eflux_yaxis
Description

Ion energy spectrogram: Number intensity is graphed against energy on the Y-axis; ranges from 30-300 keV.

Units
eV
Conversion to SI units
1.60217653e-19>J
Structure
Size
16
Elements
Index Name Valid min Valid max Fill value
1 tha_psif_en_eflux_yaxis_1 0.0 1.0E10 NaN
2 tha_psif_en_eflux_yaxis_2 0.0 1.0E10 NaN
3 tha_psif_en_eflux_yaxis_3 0.0 1.0E10 NaN
4 tha_psif_en_eflux_yaxis_4 0.0 1.0E10 NaN
5 tha_psif_en_eflux_yaxis_5 0.0 1.0E10 NaN
6 tha_psif_en_eflux_yaxis_6 0.0 1.0E10 NaN
7 tha_psif_en_eflux_yaxis_7 0.0 1.0E10 NaN
8 tha_psif_en_eflux_yaxis_8 0.0 1.0E10 NaN
9 tha_psif_en_eflux_yaxis_9 0.0 1.0E10 NaN
10 tha_psif_en_eflux_yaxis_10 0.0 1.0E10 NaN
11 tha_psif_en_eflux_yaxis_11 0.0 1.0E10 NaN
12 tha_psif_en_eflux_yaxis_12 0.0 1.0E10 NaN
13 tha_psif_en_eflux_yaxis_13 0.0 1.0E10 NaN
14 tha_psif_en_eflux_yaxis_14 0.0 1.0E10 NaN
15 tha_psif_en_eflux_yaxis_15 0.0 1.0E10 NaN
16 tha_psif_en_eflux_yaxis_16 0.0 1.0E10 NaN
Particle type
Ion
Quantity
Energy
Qualifier
Scalar

Parameter #3

Name
tha_psif_en_eflux_time
Parameter key
tha_psif_en_eflux_time
Description

tha_psif_en_eflux_time, UTC, in seconds since 01-Jan-1970 00:00:00; marks center time of data sample

Caveats

Unleaped seconds. Sample start and end time can be calculated from tha_peif_delta_time (sample duration).

Units
sec
Valid minimum
0.0
Valid maximum
5.0E9
Fill value
NaN
Parameter type
Temporal

Parameter #4

Name
tha_psif_en_eflux_delta_time
Parameter key
tha_psif_en_eflux_delta_time
Description

Duration in seconds of sample.

Units
sec
Valid minimum
0.0
Valid maximum
0.0
Fill value
NaN
Parameter type
Temporal

Parameter #5

Name
tha_psif_en_eflux_mode
Parameter key
tha_psif_en_eflux_mode
Description

SST survey mode

Valid minimum
0
Valid maximum
0
Fill value
-128
Parameter type
Other

Parameter #6

Name
SST Electron energy spectrogram
Parameter key
tha_psef_en_eflux
Description

SST Electron energy spectrogram in DSL (Despun Spacecraft) coordinates. Spectrogram data is averaged over solid angle.

Caveats

DSL coordinates: The Z-axis points towards the spacecraft spin axis and the Y-axis is obtained from the cross product of Z and the Spacecraft-Sun direction as viewed from the probe; X completes a right handed system.

Units
eV/(cm^2-s-sr-eV)
Conversion to SI units
1e4>1/(m^2*s*sr)
Coordinate system
Cartesian SR2
Structure
Size
16
Elements
Index Name Valid min Valid max Fill value
1 tha_psef_en_eflux_1 0.0 1.0E10 NaN
2 tha_psef_en_eflux_2 0.0 1.0E10 NaN
3 tha_psef_en_eflux_3 0.0 1.0E10 NaN
4 tha_psef_en_eflux_4 0.0 1.0E10 NaN
5 tha_psef_en_eflux_5 0.0 1.0E10 NaN
6 tha_psef_en_eflux_6 0.0 1.0E10 NaN
7 tha_psef_en_eflux_7 0.0 1.0E10 NaN
8 tha_psef_en_eflux_8 0.0 1.0E10 NaN
9 tha_psef_en_eflux_9 0.0 1.0E10 NaN
10 tha_psef_en_eflux_10 0.0 1.0E10 NaN
11 tha_psef_en_eflux_11 0.0 1.0E10 NaN
12 tha_psef_en_eflux_12 0.0 1.0E10 NaN
13 tha_psef_en_eflux_13 0.0 1.0E10 NaN
14 tha_psef_en_eflux_14 0.0 1.0E10 NaN
15 tha_psef_en_eflux_15 0.0 1.0E10 NaN
16 tha_psef_en_eflux_16 0.0 1.0E10 NaN
Particle type
Electron
Quantity
Number flux
Qualifier
Differential
Anisotropy

Parameter #7

Name
SST Electron energy spectrogram Y-axis (Energy).
Parameter key
tha_psef_en_eflux_yaxis
Description

Electron energy spectrogram: Number intensity is graphed against energy on the Y-axis; ranges from 30-300 keV.

Units
eV
Conversion to SI units
1.60217653e-19>J
Structure
Size
16
Elements
Index Name Valid min Valid max Fill value
1 tha_psef_en_eflux_yaxis_1 0.0 1.0E10 NaN
2 tha_psef_en_eflux_yaxis_2 0.0 1.0E10 NaN
3 tha_psef_en_eflux_yaxis_3 0.0 1.0E10 NaN
4 tha_psef_en_eflux_yaxis_4 0.0 1.0E10 NaN
5 tha_psef_en_eflux_yaxis_5 0.0 1.0E10 NaN
6 tha_psef_en_eflux_yaxis_6 0.0 1.0E10 NaN
7 tha_psef_en_eflux_yaxis_7 0.0 1.0E10 NaN
8 tha_psef_en_eflux_yaxis_8 0.0 1.0E10 NaN
9 tha_psef_en_eflux_yaxis_9 0.0 1.0E10 NaN
10 tha_psef_en_eflux_yaxis_10 0.0 1.0E10 NaN
11 tha_psef_en_eflux_yaxis_11 0.0 1.0E10 NaN
12 tha_psef_en_eflux_yaxis_12 0.0 1.0E10 NaN
13 tha_psef_en_eflux_yaxis_13 0.0 1.0E10 NaN
14 tha_psef_en_eflux_yaxis_14 0.0 1.0E10 NaN
15 tha_psef_en_eflux_yaxis_15 0.0 1.0E10 NaN
16 tha_psef_en_eflux_yaxis_16 0.0 1.0E10 NaN
Particle type
Ion
Quantity
Energy
Qualifier
Scalar

Parameter #8

Name
tha_psef_en_eflux_time
Parameter key
tha_psef_en_eflux_time
Description

tha_psef_en_eflux_time, UTC, in seconds since 01-Jan-1970 00:00:00; marks center time of data sample

Caveats

Unleaped seconds. Sample start and end time can be calculated from tha_peif_delta_time (sample duration).

Units
sec
Valid minimum
0.0
Valid maximum
5.0E9
Fill value
NaN
Parameter type
Temporal

Parameter #9

Name
tha_psif_en_flux_delta_time
Parameter key
tha_psef_en_eflux_delta_time
Description

Sample duration in seconds.

Units
sec
Valid minimum
0.0
Valid maximum
0.0
Fill value
NaN
Parameter type
Temporal

Parameter #10

Name
tha_psef_en_eflux_mode
Parameter key
tha_psef_en_eflux_mode
Description

SST survey mode

Valid minimum
0
Valid maximum
0
Fill value
-128
Parameter type
Other

SPASE version 2.0.0

Instrument: THEMIS-A: Solid State Telescope (SST): Energy flux spectrogram, electron/ion ground-calculated fluxes (30 keV - 300 keV).

Instrument ID
spase://SMWG/Instrument/THEMIS/A/SST Get XML
Name
THEMIS-A: Solid State Telescope (SST): Energy flux spectrogram, electron/ion ground-calculated fluxes (30 keV - 300 keV).
Alternate name
THEMIS-A SST
Description

THEMIS-A: The Solid State Telescope (SST), identical to that on the WIND spacecraft, measures the incoming intensity (flux per solid angle) of superthermal electrons and ions. The spacecraft is fitted with two units (heads), each SST unit has two pairs of opposing ion and electron sensors. Each single sensor covers an angle of 36 degrees. The units are oriented such that one pair is always centered in the rotation plane, the other oriented at a maximum angle of 54 degrees off the plane. Each pair of units are oriented opposite each other allowing both ion and electron sensors to sweep out a maximum of 92% of the sky. The ion and electron sensors primarily measure particles between 30-300 keV and 30-100 keV respectively with a maximum capability of 20-6000 keV and 25-1000 keV. Matched and paired electron broom magnets produce quadrapole fields reducing magnetic contamination. A mechanical attenuator is used to increase the instruments dynamical range avoiding oversaturation near the plasma sheet edge.

Additional information
THEMIS-A Spacecraft

Spacecraft description from NSSDC database

THEMIS-A Solid-State Telescope

Instrument (SST) description from NSSDC database.

Acknowledgement

NASA contract NAS5-02099, V. Angelopoulos for use of data from the THEMIS Mission, Davin Larson, and Robert P Lin for their work on the SST.

Contact
Role Person
1. Principal investigator Dr. Vassilis Angelopoulos Get XML
2. CoInvestigator Mr. Davin Larson Get XML
3. CoInvestigator Prof. Robert P. Lin Get XML
Release date
2009-05-20 21:10:04
Instrument type
Energetic Particle Instrument
Particle Detector
Investigation name
THEMIS Solid State Telescope
Observatory
THEMIS-A Get XML
Caveats

Calibration for the SST has not been completed.

SPASE version 2.0.0

Observatory: THEMIS-A

Observatory ID
spase://SMWG/Observatory/THEMIS/A Get XML
Name
THEMIS-A
Alternate name
Explorer 85
2007-004A
MIDEX/THEMIS
THEMIS-P5
30580
Description

The Time History of Events and Macroscale Interactions during Substorms (THEMIS) mission is a five-satellite Explorer mission whose primary objective is to understand the onset and macroscale evolution of magnetospheric substorms. Most importantly, THEMIS will find out which magnetotail process is responsible for substorm onset: (a) a local disruption of the plasma sheet current; or, (b) that current's interaction with the rapid influx of plasma emanating from lobe flux annihilation at ~25Re. Three inner probes at ~10Re will monitor current disruption onset, while two outer probes, at 20 and 30Re respectively, will remotely monitor plasma acceleration due to lobe flux dissipation. The five small satellites were launched together on a Delta II rocket and they carry identical sets of instruments including an electric field instrument (EFI), a flux gate magnetometer (FGM), a search coil magnetometer (SCM), a electro-static analyzer, and solid state telescopes (SST). The mission consists of several phases. In the first phase, the spacecraft will all orbit as a tight cluster in the same orbital plane with apogee at 15.4 Earth radii (RE). In the second phase, also called the Dawn Phase, the satellites will be placed in their orbits and during this time their apogees will be on the dawn side of the magnetosphere. During the third phase (also known as the Tail Science Phase) the apogees will be in the magnetotail. The fourth phase is called the Dusk Phase or Radiation Belt Science Phase, with all apogees on the dusk side. In the fifth and final phase, the apogees will shift to the sunward side (Dayside Science Phase).

All five satellites will have similar perigee altitudes (1.16-1.5 Re) but varying apogee altitudes (P1: ~30 RE, P2: ~20 RE, P3 & P4: ~12 RE, P5: ~10RE) with corresponding orbital periods of ~4, 2, and 1 days, respectively. This results in multi-point magnetic conjunctions. Every four days the satellites will line up along the Earth's magnetic tail with magnetic foot points in the North American sector, allowing the tracking of disturbances through different geospace regions from tail to ground.

The satellite data will be combined with observations of the aurora from a network of 20 ground observatories (all sky imagers, magnetometers) across the North American continent. In addition to its primary goal, THEMIS will answer critical questions in radiation belt physics and solar wind - magnetosphere energy coupling. THEMIS is complementary to MMS in terms of the temporal and spatial scales of the phenomena observed by these two constellation missions. THEMIS's focus is macroscale, whereas MMS will observe micro/meso scale features.

Additional information
Time History of Events and Macroscale Interactions during Substorms (THEMIS) mission

THEMIS Mission Homepage

Information on Time History of Events and Macroscale Interactions during Substorms (THEMIS) mission

NSSDC Master Catalog information on the THEMIS Mission

Acknowledgement

National Aeronautics and Space Administration/United States

Contact
Role Person
1. Principal investigator Dr. Vassilis Angelopoulos Get XML
2. Project scientist Dr. David G. Sibeck Get XML
Release date
2009-05-20 20:00:12
Prior ID
spase://SMWG/Observatory/THEMIS-A
Observatory group
THEMIS
Location
Region
Earth.Magnetosheath
Earth.Magnetosphere.Magnetotail
Earth.Magnetosphere.Main
Heliosphere.NearEarth

SPASE version 2.0.0

Person: Dr. Vassilis Angelopoulos

Name
Dr. Vassilis Angelopoulos
Organization
University of California, Los Angeles
Email
vassilis@igpp.ucla.edu
vassilis@ssl.berkeley.edu
Phone
+1-310-794-7090
+1-510-643-1871
Person ID
spase://SMWG/Person/Vassilis.Angelopoulos Get XML
Release date
2008-03-11 19:28:45

SPASE version 2.0.0

Person: Mr. Davin Larson

Name
Mr. Davin Larson
Organization
University of California, Berkeley
Person ID
spase://SMWG/Person/Davin.Larson Get XML

SPASE version 2.0.0

Person: Prof. Robert P. Lin

Name
Prof. Robert P. Lin
Organization
University of California, Berkeley
Email
rlin@ssl.berkeley.edu
Phone
+1-510-642-1149
Person ID
spase://SMWG/Person/Robert.P.Lin Get XML
Release date
1999-08-18 00:00:00

SPASE version 2.0.0

Person: Dr. Robert E. McGuire

Name
Dr. Robert E. McGuire
Organization
NASA Goddard Space Flight Center
Address
Code 672, Greenbelt, MD 20771, USA
Email
mcguire@mail630.gsfc.nasa.gov
Phone
1-301-286-7794
Person ID
spase://SMWG/Person/Robert.E.McGuire Get XML
Release date
2007-05-30 15:25:24

SPASE version 2.0.0

Person: Dr. David G. Sibeck

Name
Dr. David G. Sibeck
Organization
NASA/GSFC, Code 672
Person ID
spase://SMWG/Person/David.G.Sibeck Get XML

SPASE version 1.2.0

Repository: CDAWeb Data Repository FTP Interface

Repository ID
spase://SMWG/Repository/NASA/GSFC/SPDF/CDAWeb Get XML
Name
CDAWeb Data Repository FTP Interface
Description

Coordinated Data Analysis Web (CDAWeb) supports not only interactive plotting of variables from multiple instruments on multiple investigations simultaneously on arbitrary, user-defined time-scales. It also supports data retrieval in various formats using its interactive web interface or ftp service.

Additional information
CDAWeb Home Page

Coordinated Data Analysis Web (CDAWeb) home page at Space Physics Data Facility of the NASA Goddard Space Flight Center.

Contact
Role Person
1. Project scientist Dr. Robert E. McGuire Get XML
Release date
2008-08-26 21:14:34
Prior ID
spase://VMO/Repository/CDAWeb