This page summarizes information about the selected resource and its origin based on SPASE metadata.
SPASE version 2.0.0
H+, O+, He+ and He++ number fluxes for survey purposes only
Reference:E.G. Shelley et al., The Toroidal Imaging Mass-Angle Spectrograph (TIMAS) for the Polar Mission, Sp. Sci. Rev, Vol 71, pp 497-530, 1995.
Version 0: June, 2001
A PAPCO module for reading and displaying TIMAS (and other POLAR) data.
PaPCo is IDL software for data visualization and analysis. It is modular, PaPCo modules built by various institutions and individuals plug into PaPCo core to provide data products. These modules provide graphic panels that are stacked on a time axis. About 60 modules exist, and 30 are supported as “core modules” that come with PaPCo. There are modules from 15+ spacecraft, including CRRES, Polar, Cassini and Cluster. Data from CDAWeb is plottable as well. The software is open-source, making it very flexible and well-suited for science use.
| Role | Person | |
|---|---|---|
| 1. | Principal investigator | Dr. W. K. Peterson |
FTP repository of Polar TIMAS key parameter data in CDF format at CDAWeb
On December 8, 1998 the TIMAS instrument had a high voltage breakdown that resulted in a loss of sensitivity at energies above 700 eV/q and non linear response to ion fluxes at energies below 700 eV/q. The data from the two lowest energy channels in this data set (430 and 585 eV respectively) should be used with caution. Prior to the breakdown, the TIMAS H0 data product provides higher time resolution data in the full energy and angular range.
The K1 data are averaged over time (96 seconds) and angle (nearly the full 4 pi), so narrow angular and/or temporal features are not shown. Higher temporal and angular resolution data can be interactively generated at http://lasp.colorado.edu/timas/mrdf/
NSSDC standard-reference time value (UT) at the center of the accumulation interval.
H+ number flux integrated over all pitch angles; depends on 'Epoch' and 'energy'.
| Bin | Band name | Low energy | High energy |
|---|---|---|---|
| 1 | Flux 430 eV/e | 369.2 | 491.0 |
| 2 | Flux 585 eV/e | 508.1 | 661.5 |
| 3 | Flux 795 eV/e | 699.2 | 891.4 |
| 4 | Flux 1.1 keV/e | 962.1 | 1200.9 |
| 5 | Flux 1.5 keV/e | 1323.6 | 1617.8 |
| 6 | Flux 2.0 keV/e | 1820.8 | 2179.2 |
| 7 | Flux 2.4 keV/e | 2228.5 | 2647.5 |
| 8 | Flux 3.0 keV/e | 2733.1 | 3210.9 |
| 9 | Flux 3.6 keV/e | 3358.0 | 3887.8 |
| 10 | Flux 4.4 keV/e | 4119.7 | 4713.1 |
| 11 | Flux 5.4 keV/e | 5048.3 | 5718.9 |
| 12 | Flux 6.6 keV/e | 6180.2 | 6945.2 |
| 13 | Flux 8.0 keV/e | 7560.0 | 8440.0 |
| 14 | Flux 9.8 keV/e | 9242.0 | 10262.2 |
| 15 | Flux 12 keV/e | 11313.3 | 12462.7 |
| 16 | Flux 15 keV/e | 13823.7 | 15159.5 |
| 17 | Flux 18 keV/e | 16894.5 | 18436.3 |
| 18 | Flux 21.5 keV/e | 20619.7 | 22449.1 |
O+ number flux integrated over all pitch angles; depends on 'Epoch' and 'energy'.
| Bin | Band name | Low energy | High energy |
|---|---|---|---|
| 1 | Flux 430 eV/e | 369.2 | 491.0 |
| 2 | Flux 585 eV/e | 508.1 | 661.5 |
| 3 | Flux 795 eV/e | 699.2 | 891.4 |
| 4 | Flux 1.1 keV/e | 962.1 | 1200.9 |
| 5 | Flux 1.5 keV/e | 1323.6 | 1617.8 |
| 6 | Flux 2.0 keV/e | 1820.8 | 2179.2 |
| 7 | Flux 2.4 keV/e | 2228.5 | 2647.5 |
| 8 | Flux 3.0 keV/e | 2733.1 | 3210.9 |
| 9 | Flux 3.6 keV/e | 3358.0 | 3887.8 |
| 10 | Flux 4.4 keV/e | 4119.7 | 4713.1 |
| 11 | Flux 5.4 keV/e | 5048.3 | 5718.9 |
| 12 | Flux 6.6 keV/e | 6180.2 | 6945.2 |
| 13 | Flux 8.0 keV/e | 7560.0 | 8440.0 |
| 14 | Flux 9.8 keV/e | 9242.0 | 10262.2 |
| 15 | Flux 12 keV/e | 11313.3 | 12462.7 |
| 16 | Flux 15 keV/e | 13823.7 | 15159.5 |
| 17 | Flux 18 keV/e | 16894.5 | 18436.3 |
| 18 | Flux 21.5 keV/e | 20619.7 | 22449.1 |
He+ number flux integrated over all pitch angles; depends on 'Epoch' and 'energy'.
| Bin | Band name | Low energy | High energy |
|---|---|---|---|
| 1 | Flux 430 eV/e | 369.2 | 491.0 |
| 2 | Flux 585 eV/e | 508.1 | 661.5 |
| 3 | Flux 795 eV/e | 699.2 | 891.4 |
| 4 | Flux 1.1 keV/e | 962.1 | 1200.9 |
| 5 | Flux 1.5 keV/e | 1323.6 | 1617.8 |
| 6 | Flux 2.0 keV/e | 1820.8 | 2179.2 |
| 7 | Flux 2.4 keV/e | 2228.5 | 2647.5 |
| 8 | Flux 3.0 keV/e | 2733.1 | 3210.9 |
| 9 | Flux 3.6 keV/e | 3358.0 | 3887.8 |
| 10 | Flux 4.4 keV/e | 4119.7 | 4713.1 |
| 11 | Flux 5.4 keV/e | 5048.3 | 5718.9 |
| 12 | Flux 6.6 keV/e | 6180.2 | 6945.2 |
| 13 | Flux 8.0 keV/e | 7560.0 | 8440.0 |
| 14 | Flux 9.8 keV/e | 9242.0 | 10262.2 |
| 15 | Flux 12 keV/e | 11313.3 | 12462.7 |
| 16 | Flux 15 keV/e | 13823.7 | 15159.5 |
| 17 | Flux 18 keV/e | 16894.5 | 18436.3 |
| 18 | Flux 21.5 keV/e | 20619.7 | 22449.1 |
He++ number flux integrated over all pitch angles; depends on 'Epoch' and 'energy'.
| Bin | Band name | Low energy | High energy |
|---|---|---|---|
| 1 | Flux 430 eV/e | 369.2 | 491.0 |
| 2 | Flux 585 eV/e | 508.1 | 661.5 |
| 3 | Flux 795 eV/e | 699.2 | 891.4 |
| 4 | Flux 1.1 keV/e | 962.1 | 1200.9 |
| 5 | Flux 1.5 keV/e | 1323.6 | 1617.8 |
| 6 | Flux 2.0 keV/e | 1820.8 | 2179.2 |
| 7 | Flux 2.4 keV/e | 2228.5 | 2647.5 |
| 8 | Flux 3.0 keV/e | 2733.1 | 3210.9 |
| 9 | Flux 3.6 keV/e | 3358.0 | 3887.8 |
| 10 | Flux 4.4 keV/e | 4119.7 | 4713.1 |
| 11 | Flux 5.4 keV/e | 5048.3 | 5718.9 |
| 12 | Flux 6.6 keV/e | 6180.2 | 6945.2 |
| 13 | Flux 8.0 keV/e | 7560.0 | 8440.0 |
| 14 | Flux 9.8 keV/e | 9242.0 | 10262.2 |
| 15 | Flux 12 keV/e | 11313.3 | 12462.7 |
| 16 | Flux 15 keV/e | 13823.7 | 15159.5 |
| 17 | Flux 18 keV/e | 16894.5 | 18436.3 |
| 18 | Flux 21.5 keV/e | 20619.7 | 22449.1 |
Total Background counts per spin
Energy bin values ABOVE space craft potential
SPASE version 2.0.0
This investigation onboard POLAR spacecraft utilizes a toroidal ion mass spectrograph (TIMS) to fulfill its objectives, which are to study (1) the properties, location, and morphology of the principal source region for the entry of solar wind plasma into the magnetosphere, i.e., the polar cusp; (2) the properties, location, and morphology of the principal source region for hot ionospheric plasma in the magnetosphere, i.e., the auroral acceleration region; (3) the details of the processes by which the source plasmas are injected into trapped orbits, with special emphasis on the mass dependence of these processes; (4) details of the processes by which relatively cool source plasmas are energized into hot plasma, with special emphasis on the mass dependence of these processes; and (5) the details of the processes by which the hot magnetospheric plasma are lost, for example through wave-particle scattering and charge exchange, with special emphasis on the mass dependence of these processes.
The Toroidal Imaging Mass-Angle Spectrograph (TIMAS) instrument measures the full three-dimensional velocity distribution functions of all major magnetospheric ion species with one-half spin period time resolution. The TIMAS is a first order double focusing (angle and energy), imaging spectrograph that simultaneously measures all mass per charge components from 1 AMU/e to greater than 32 AMU/e over a nearly 360 degrees by 10 degree instantaneous field-of-view in 20 milliseconds. Mass per charge is dispersed radially on an anular microchannel plate detector and the azimuthal position on the detector is a map of the instantaneous 360 degrees field of view. With the rotation of the spacecraft, the TIMAS sweeps out a 4pi solid angle image in a half spin period. The energy per charge range from 15eV/e to 32 keV/e is covered in 28 non-contiguous steps spaced approximately logarithmically with adjacent steps separated by about 30%. In order to handle the large volume of data within the telemetry limitations the distributions are compressed to varying degrees in angle and energy, log-count compressed and then further compressed by a lossless technique. This data processing task is supported by two SA3300 microprocessors. The voltages (up to + 5 kV) for the tandem toroidal electrostatic analyzers are supplied from common high voltage supplies using optically controlled series-shunt regulators.
Full and detailed descriptions of the TIMAS instrument goals, design and calibration (written in 1996).
Information about the Toroidal Imaging Mass-Angle Spectrograph (TIMAS) experiment on the POLAR mission.
| Role | Person | |
|---|---|---|
| 1. | Principal investigator | Dr. W. K. Peterson |
SPASE version 2.0.0
POLAR is one of four spacecraft in the Global Geospace Science (GGS) program. These are among the six spacecraft in the International Solar Terrestrial Physics (ISTP) program. POLAR provides multi-wavelength imaging of the aurora, measuring plasma entry into the polar magnetosphere and geomagnetic tail, the flow of plasmas to and from the ionosphere, and the deposition of particle energy in the ionosphere and upper atmosphere. POLAR has on-board propulsion systems and a design lifetime of three to five years, with redundant subsystems. POLAR is cylindrical, approximately 2.8 m in diameter by 1.25 m high (plus 1.25 m for its two despun platforms), with body-mounted solar cells, weighs 1250 kg and uses 333 W of power. The spin rate is 10 rpm around an axis approximately normal to the orbital plane. It has long wire spin-plane antennas, inertial booms, and spin-plane appendages to support sensors. POLAR has two despun gimbaled instrument platforms, and booms are deployed along both Z axes. Data are stored using on-board tape recorders and are relayed to the Deep Space Network at 600 kbps maximum (250 kbps nominal) although the average real-time data rate for POLAR is 41.6 kbps. POLAR has a 22.6-h polar orbit (90 deg inclination), with perigee and apogee of 11,500 and 57,000 km. Polar was launched to observe the polar magnetosphere and, as its orbit has precessed with time, has observed the equatorial inner magnetosphere and is now carrying out an extended period of southern hemisphere coverage. Details on the POLAR mission and instrumentation are provided in Space Science Reviews (Vol. 71, Nos. 1-4, 1995) and reprinted in The Global Geospace Mission, edited by C. T. Russell (Kluwer, 1995).
Web site of NASA Polar Mission, including overview, data products, FTP to the data, publications, educational outreach, orbits, instrument descriptions, contacts, news archive, and ISTP archive.
Information about the Polar mission
| Role | Person | |
|---|---|---|
| 1. | Project scientist | Dr. John B. Sigwarth |
SPASE version 2.0.0
SPASE version 2.0.0
SPASE version 2.0.0
SPASE version 1.2.0
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.
Coordinated Data Analysis Web (CDAWeb) home page at Space Physics Data Facility of the NASA Goddard Space Flight Center.
| Role | Person | |
|---|---|---|
| 1. | Project scientist | Dr. Robert E. McGuire |