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  4. Observatory
  5. Persons

Numerical Data Product: THEMIS-B: Probe Electric Field Instrument and Search Coil Magnetometer Instrument, Digital Fields Board - digitally computed Filter Bank spectra and E12 peak and average in HF band.

Resource ID spase://VMO/NumericalData/THEMIS/B/FBK/PT4S Get XML
Name THEMIS-B: Probe Electric Field Instrument and Search Coil Magnetometer Instrument, Digital Fields Board - digitally computed Filter Bank spectra and E12 peak and average in HF band.
Description The Filter Bank is part of the Digital fields board and provides band-pass filtering for EFI and SCM spectra as well as E12HF peak and average value calculations. The Filter Bank provides band-pass filtering for less computationally and power intensive spectra than the FFT would provide. The process is as follows: Signals are fed to the Filter Bank via a low-pass FIR filter with a cut-off frequency half that of the original signal maximum. The output is passed to the band-pass filters, is differenced from the original signal, then absolute value of the data is taken and averaged. The output from the low-pass filter is also sent to a second FIR filter with 2:1 decimation. This output is then fed back through the system. The process runs through 12 cascades for input at 8,192 samples/s and 13 for input at 16,384 samples/sec (EAC input only), reducing the signal and computing power by a factor 2 at each cascade. At each cascade a set of data is produced at a sampling frequency of 2^n from 2 Hz to the initial sampling frequency (frequency characteristics for each step are shown below in Table 1). The average from the Filter Bank is compressed to 8 bits with a pseudo-logarithmic encoder. The data is stored in sets of six frequency bins at 2.689 kHz, 572 Hz, 144.2 Hz, 36.2 Hz, 9.05 Hz, and 2.26 Hz. The average of the coupled E12HF signal and it's peak value are recorded over 62.5 ms windows (i.e. a 16 Hz sampling rate). Accumulation of values from signal 31.25 ms windows is performed externally. The analog signals fed into the FBK are E12DC and SCM1. Sensor and electronics design provided by UCB (J. W. Bonnell, F. S. Mozer), Digital Fields Board provided by LASP (R. Ergun), Search coil data provided by CETP (A. Roux). Table 1: Frequency Properties. Cascade | Frequency content of Input Signal | Low-pass Filter Cutoff Frequency | Freuency Content of Low-pass Output Signal | Filter Bank Frequency Band 0* 0 - 8 kHz 4 kHz 0 - 4 kHz 4 - 8 kHz 1 0 - 4 kHz 2 kHz 0 - 2 kHz 2 - 4 kHz 2 0 - 2 kHz 1 kHz 0 - 1 kHz 1 - 2 kHz 3 0 - 1 kHz 512 Hz 0 - 512 Hz 512 Hz - 1 kHz 4 0 - 512 Hz 256 Hz 0 - 256 Hz 256 - 512 Hz 5 0 - 256 Hz 128 Hz 0 - 128 Hz 128 - 256 Hz 6 0 - 128 Hz 64 Hz 0 - 64 Hz 64 - 128 Hz 7 0 - 64 Hz 32 Hz 0 - 32 Hz 32 - 64 Hz 8 0 - 32 Hz 16 Hz 0 - 16 Hz 16 - 32 Hz 9 0 - 16 Hz 8 Hz 0 - 8 Hz 8 - 16 Hz 10 0 - 8 Hz 4 Hz 0 - 4 Hz 4 - 8 Hz 11 0 - 4 Hz 2 Hz 0 - 2 Hz 2 - 4 Hz 12 0 - 2 Hz 1 Hz 0 - 1 Hz 1 - 2 Hz *Only available for 16,384 Hz sampling.
Acknowledgement NASA Contract NAS5-02099
Contact
Role Person
1. Principal investigator
Dr. Vassilis Angelopoulos Get XML
2. CoInvestigator
John W. Bonnell Get XML
3. CoInvestigator
Dr. Robert E. Ergun Get XML
4. CoInvestigator
Prof. Forrest S. Mozer Get XML
5. CoInvestigator
Dr. Alain Roux Get XML
Release date 2008-12-06 01:08:40
Repository
Name CDAWeb Data Repository FTP Interface Get XML
Availability Online
Access rights Open
URL
CDAWeb FTP Access NASA/GSFC CDAWeb ftp access to FBK data.
Format CDF
Provider version xxxx
Instruments THEMIS-B Electric Field Instrument Get XML
THEMIS-B: Search Coil Magnetometer Get XML
Measurement type Electric field
Magnetic field
Spectrum
Temporal description
Start date 2007-02-24 00:00:01
Relative stop date -P7D
Cadence PT4S

Instrument: THEMIS-B Electric Field Instrument

Instrument ID spase://SMWG/Instrument/THEMIS/B/EFI Get XML
Name THEMIS-B Electric Field Instrument
Alternate name THEMIS-B EFI
Description The Electric Field Instrument (EFI) on the THEMIS spacecraft measures the three components of the ambient vector electric field. Measurements are performed using four wire spin plane booms and two rigid axial booms. Waveform measurements cover DC up to 4 kHz (with AC-coupled differential measurements from ~10 Hz up to 8 kHz), with on-board spectral measurements covering the same ranges, as well as providing an estimate of integrated power in the 100- to 400-kHz band. On-board spin-fit E-field estimates are also provided for both the spin plane and axial measurements. On-board estimates of the spacecraft floating potential are also produced for use in particle moment calculations and burst trigger evaluations. Both individual (Vn, n=1..6) and differential (Emn = Vm – Vn, m,n = [(1,2), (3,4), (5,6)]) sensor potentials are measured. Booms 1 & 2 are in the spin plane and have a length from tip to tip of 49.6 meters. Booms 3 & 4 are in the spin plane and have a length from tip to tip of 40.4 meters. Booms 5 & 6 are the axial booms and have a length from tip to tip of 5.63 meters. The differential sensor potentials are used to estimate the ambient vector E-field. The individual sensor potentials are used to verify proper sensor operation, estimate the spacecraft floating potential, and measure the ambient plasma density with high (sub-spin-period) time resolution. Ground based electric field magnitude and direction measurements are provided with the Z component, with the Z component removed, and with the Z component estimated using the E.B=0 equality. The data are provided in DSL (despun spacecraft L-Z vector), GSM, and GSE coordinates.
Additional information
THEMIS-B Electric Fields Instrument Instrument description from NSSDC database
Acknowledgement NASA contract NAS5-02099 and V. Angelopoulos for use of data from the THEMIS Mission. Specifically: J. W. Bonnell and F. S. Mozer for use of EFI data.
Contact
Role Person
1. Principal investigator
Dr. Vassilis Angelopoulos Get XML
2. CoInvestigator
John W. Bonnell Get XML
3. CoInvestigator
Prof. Forrest S. Mozer Get XML
Release date 2008-12-05 02:24:47
Prior ID spase://SMWG/Instrument/THEMIS-B/EFI Get XML
Instrument type Antenna
DoubleSphere
Investigation name THEMIS Electric Fields Instrument
Observatory THEMIS-B Get XML
Caveats Measurements on the axial booms(5 & 6) may have large errors due to their proximity to the spacecraft (the axial booms are much shorter than other booms). The spin plane booms for THEMIS B were not deployed until November 17, 2007 at 0600 UT, any EFI measurements before this date should not be used.

Instrument: THEMIS-B: Search Coil Magnetometer

Instrument ID spase://SMWG/Instrument/THEMIS/B/SCM Get XML
Name THEMIS-B: Search Coil Magnetometer
Alternate name THEMIS-B SCM
Description THEMIS-B Search Coil Magnetometer for measuring three dimensional changes in magnetic flux between 0.1 Hz and 4 kHz; the range extending to 8 kHz under certain conditions. The instrument is mounted on a ridged, retractable boom one meter in length extending from the top corner of the spacecraft (positive y-axis, negative x-axis in SPG coordinates). The SCM boom deploys at an angle of -167.9 degrees from the x-axis (SPG) and 10.1 degrees above the spin plane. Two of the probe's sensors are aligned within the spin plane of the spacecraft, with the B_x component 12.1 degrees from the SPG x-axis, the third being parallel to the spin axis completing a right handed orthogonal system. The three sensors are composed of two windings surrounding a core with a high magnetic permeability. The main winding, used for detection, consists of 51600 turns; the secondary winding introduces a flux feedback to damped the frequency response of the sensor and keep it independent of temperature variation. Multi-Layer Insulation keeps the probe thermally insulated while electrostatic shielding reduces its sensitivity to electric fields. Low noise at slower frewencies allows for sufficient overlap with Fluxgate Magnetomer (FGM) measurements (noise less than 0.76 pT/sqrt(Hz) at 10 Hz). Data from the SCM is passed through three pre-amplifiers, one for each sensor component, before going on to the DFB and IDPU for processing and digitization. Survey modes for the SCM are listed below in Table 1. Table 1: SCM Telemetry Modes. Filter Bank (fbk)*: Mean signal value over 6 frequency bands (4-2 kHz, 1-0.5 kHz, 256-128 Hz, 64-32 Hz, 16-8 Hz, 4-2 Hz); sampling rate of 1/16 to 8 S/s. Fast Survey (scf): Waveform data for the 3 SCM components; sampling rate between 2 and 256 S/s, nominal value is 8. Particle Burst (scp): Waveform data nominally at 128 S/s. Wave Burst (scw): Waveform data nominally at 8192 S/s. Particle Burst Spectra (ffp)**: Compressed FFT spectra in 16, 32, or 64 frequency bins; sampling between 1/4 to 8 S/s. Wave Burst Spectra (ffw)**: Compressed FFT spectra in 16, 32, or 64 frequency bins; sampling between 1/4 to 8 S/s. *Only two available inputs between all 3 SCM and 12 EFI data signals. **Only four available inputs between 3 SCM and 16 other data signals.
Additional information
THEMIS Home Page THEMIS Home Page.
THEMIS-B Spacecraft Spacecraft description from NSSDC database
THEMIS-B Search Coil Magnetometer Instrument (SCM) description from NSSDC database.
The Search Coil Magnetometer for THEMIS A. Roux et. al. In depth description of the THEMIS SCM.
Acknowledgement NASA contract NAS5-02099, V. Angelopoulos for use of data from the THEMIS Mission; also A. Roux and CETP for their work on the SCM.
Contact
Role Person
1. Principal investigator
Dr. Vassilis Angelopoulos Get XML
2. CoInvestigator
Dr. Alain Roux Get XML
Release date 2008-12-09 21:38:17
Instrument type Magnetometer
SearchCoil
Investigation name THEMIS Search Coil Magnetometer
Observatory THEMIS-B Get XML

Observatory: THEMIS-B

Observatory ID spase://SMWG/Observatory/THEMIS/B Get XML
Name THEMIS-B
Alternate names Explorer 86
2007-004B
MIDEX/THEMIS
THEMIS-P1
30581
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 2008-11-11 22:24:55
Prior ID spase://SMWG/Observatory/THEMIS-B Get XML
Observatory group THEMIS
Location
Region Earth.Magnetosheath
Earth.Magnetosphere.Magnetotail
Earth.Magnetosphere.Main
Heliosphere.NearEarth

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

Person: John W. Bonnell

Name John W. Bonnell
Organization University of California, Berkeley
Address University of California, Berkeley Space Sciences Lab 7 Gauss Way Berkeley, CA 94720-7450, Annex 7
Email jbonnell@ssl.berkeley.edu
Phone 510-642-0852
Person ID spase://SMWG/Person/John.W.Bonnell Get XML

Person: Dr. Robert E. Ergun

Name Dr. Robert E. Ergun
Organization University of Colorado
Person ID spase://SMWG/Person/Robert.E.Ergun Get XML

Person: Prof. Forrest S. Mozer

Name Prof. Forrest S. Mozer
Organization University of California, Berkeley
Address Room 306 Space Science Laboratory University of California, Berkeley Berkeley CA 94720
Email mozer@sunspot.ssl.berkeley.edu
Phone +1-510-642-0549
Person ID spase://SMWG/Person/Forrest.S.Mozer Get XML
Release date 2008-08-26 18:43:16

Person: Dr. Alain Roux

Name Dr. Alain Roux
Organization CNRS Centre de Recherches en Physique de L Environ
Person ID spase://SMWG/Person/Alain.Roux Get XML

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

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

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 Get XML

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