This page summarizes information about the selected resource and its origin based on SPASE metadata.
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RPI passive wave measurement capturing voltage spectral density of the radio emissions in space as a function of frequency, typically between 3 and 1009 kHz. This operating frequency range was selected by the RPI team to provide optimal temporal resolution of the wave observations. Commonly used in the analysis of noise generators, spectral density is a frequency-dependent characteristic that describes how much power is generated by the emission source in a 1 Hz bandwidth. The original description of emissions was done in terms of thermal noise measurements, though the same approach also applies to non-thermal emissions such as AKR. CDF_DS_PT5M stores calibrated data from all three RPI antennas X, Y, and Z individually and a combined X+Y antenna channel. The data are presented as the Voltage Spectral Density (VSD), which is the root of power spectral density, measured in [V/root-Hz] units. Note that conversion of antenna voltage to electric field strength depends on the effective length of the receive antenna, and such conversion is not performed here. (See spase://SMWG/Instrument/IMAGE/RPI for a time history of the lengths of the three mutually orthogonal RPI dipole antennas.) RPI is capable of detecting input radio emissions above its noise floor of 5 nV/root-Hz, which is determined by the internal white noise of the RPI antenna pre-amplifiers. The VSD in RPI spectrogram data is presented in dB relative to 1 V/root-Hz (logarithmic scale), units of dB(V/root-Hz). The RPI instrument noise floor is 5 nV/root-Hz = -166 dB(V/root-Hz) at the receiver input. Software suggested by the science team for CDF file visualization: (1) Plotting tool at the CDAWeb portal, (2) For analysis beyond static image inspection, including color scale optimization, zooming, text export, alternative data representations in physical units, detailed frequency and time information, overlaid model fpe and fce graphs, and EPS quality figures, use BinBrowser software at UML, http://ulcar.uml.edu/rpi.html
IMAGE RPI Instrument page maintained by NASA GSFC with RPI facts, description, team, data, documents, discoveries, and related links sections
IMAGE RPI Instrument page maintained by University of Massachusetts Lowell with RPI description, team, software downloads, software user guides, access to CORPRAL automated prospecting results, mission planning tools and commanding guide, data model descriptions for Level 0 and 1, sonification files of 2003 Halloween storm, and useful links
RPIAnywhere software download page, including BinBrowser (RPI data analysis tool) and EdRPI (RPI mission planning tool)
Users please acknowledge Coordinated Data Analysis Web (CDAWeb) at the NASA Goddard Space Flight Center and RPI Principal Investigator Prof. B. W. Reinisch of the University of Massachusetts Lowell for making these CDF files available.
| Role | Person | |
|---|---|---|
| 1. | Principal investigator | Prof. Bodo W. Reinisch |
| 2. | Data producer Technical contact |
Dr. Ivan A. Galkin |
FTP access to repository of IMAGE RPI passive wave measurements (dynamic spectrograms) in CDF format at NASA CDAWeb.
Repository of IMAGE RPI passive wave measurements (dynamic spectrograms) in CDF format at NASA CDAWeb, accessible via web interface. Name of the data resource: IM_K1_RPI.
Users please acknowledge Coordinated Data Analysis Web (CDAWeb) at the NASA Goddard Space Flight Center and RPI Principal Investigator Prof. B. W. Reinisch of the University of Massachusetts Lowell for making these CDF files available.
In Cadence below, the 5 minutes refers to the nominal interval between measurements. Actual cadence of passive measurement varied between 3 to 6 minutes depending on the RPI science plan and design of measurement schedules.
(A) Known artifacts of dynamic spectrograms are (1) a horizontal line at 20 kHz where the frequency stepping changes from linear to logarithmic, and (2) a variety of interference sources internal to the IMAGE observatory appear as horizontal lines on the dynamic spectrograms including, most prominently, 101 kHz; additional lines appear at 63 kHz and its 126 kHz 2nd harmonic (battery charger), at times a broad band is also present between 160 and 200 kHz due to the torque rod operation, and a narrow line appears at 75 kHz due to the S-band transponder. Other known intereferer lines are 150 kHz, 200 kHz, and 240 kHz (deck plate heaters and other onboard instruments), but these lines are usually not present in the measurement. (B) When the spectrogram is plotted, the pixel size is made wide enough to fill the gaps caused by the 5 minute cadence of the measurements. (C) Comparison of voltage spectral density with other space receiver data has to consider differences in the antenna configurations.
Commonly used in circuit analysis, Power Spectral Density (PSD) describes how much noise power is generated by the emission source in a 1 Hz bandwidth. Dynamic Specrtograms use Voltage Spectral Density (VSD), which is root of PSD, measured in V/root-Hz units. The VSD in RPI spectrograms is presented in dB relative to 1 V/root-Hz (logarithmic scale), units of dB(V/root-Hz). On average, the RPI instrument noise floor is 5 nV/root-Hz = -166 dB(V/root-Hz) at the receiver input.
One measurement is an array of voltage spectral density (VSD) values, as functions of frequency, obtained during the frequency sweep. For each operating frequency, four values of VSD are reported: (1) antenna X, (2) antenna Y, (3) antenna Z, (4) combined antennas X and Y to remove spacecraft spin modulation. Resulting structure is a linear 256 x 4 array. Number of frequencies for which the voltage spectral density values are given depends on the choice of frequency sweep (see "List of Frequencies" and "Number of Frequencies" parameters and their description below). The "256" value stated in Size is the upper limit. Note that Index "0" means a wild card ("don't care"), index "-1" means the whole dimension.
| Index | Name | Parameter key | Units | Valid min | Valid max | Fill value |
|---|---|---|---|---|---|---|
| -1 0 | Frequency Dimension | Frequency | ||||
| 0 -1 | Antenna Dimension | |||||
| 0 1 | Voltage Spectral Density in antenna X | Amplitude_X | dB(V/root-Hz) | -190 | -70 | -1.0e+031 |
| 0 2 | Voltage Spectral Density in antenna Y | Amplitude_Y | dB(V/root-Hz) | -190 | -70 | -1.0e+031 |
| 0 3 | Voltage Spectral Density in antenna Z | Amplitude_Z | dB(V/root-Hz) | -190 | -70 | -1.0e+031 |
| 0 4 | Voltage Spectral Density in combined antennas X and Y | Amplitude_XY | dB(V/root-Hz) | -190 | -70 | -1.0e+031 |
List of operating frequencies at which sample data were collected to obtain VSD values. Actual frequency values vary from measurement to measurement depending on the choice of frequency sweep. Early in the mission, a variety of frequency sweeps were tested until March 27, 2001 when they were streamlined to three basic types: PROGRAM-23: linear sweep from 3 to 20 kHz with 400 Hz step (13 sec running time), PROGRAM-26: logarithmic sweep from 20 to 1009 kHz with 2% stepping (59 sec running time), and PROGRAM-25: logarithmic sweep from 20 to 300 kHz with 2% stepping (37 sec running time). Most commonly used since April 2001, PROGRAM-23 and PROGRAM-26 combination takes 72 sec to complete one sweep from 3 to 1009 kHz. Other frequency sweeps were also exercised, in addition to the three basic types, during experiments on detection of signals from the ground VLF transmitters. For a greater detail on the RPI measurement programming cases in the dynamic spectrogram mode, please refer to RPI operational logs available as part of the RPIAnywhere software package at http://ulcar.uml.edu/rpi.html.
Linear 1D array of frequency values, up to 256. Actual number of frequencies for which the voltage spectral density values were measured depends on the choice of frequency sweep (see "Number of Frequencies" parameter and its description below). The "256" value stated in Size is the upper limit.
| Index | Name | Valid min | Valid max | Fill value |
|---|---|---|---|---|
| -1 | Frequency | 3 | 3000 | -1.0e+031 |
Number of frequencies in the sweep, see "List of Frequencies"
Epoch timestamp of the beginning of the spectrogram measurement. Use Measurement Duration to obtain time of measurement stop.
The 5 minutes refers to the nominal interval between measurements. Actual cadence of passive measurement varied between 3 to 6 minutes depending on the RPI science plan and design of measurement schedules.
Duration of one spectrogram measurement.
Number of looks at each of the spectrogram frequencies, encoded. Encoding: stored number N is used as power of 2 (i.e., 2**N is actual number of repetitions)
Instrument setting describing receiver gains in X/Y and Z channels, encoded. See data model description at http://ulcar.uml.edu/rpi.html for additional details on base gain decoding procedure.
List of 25 parameter values that specify RPI instrument configuration during the measurement. For further detail on parameter value interpretation see data model description document at http://ulcar.uml.edu/rpi.html.
Linear 1D array of values used to configure RPI instrument for a measurement mode.
| Index | Name |
|---|---|
| -1 | RPI Parameter |
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The main science objective of the Radio Plasma Imager (RPI) was to characterize plasma in the Earth's magnetosphere utilizing imaging in the radio frequency range.
The RPI on the IMAGE spacecraft was a pioneering instrument designed as a low frequency (3 kHz to 3 MHz) long-range magnetospheric radio sounder, relaxation sounder, and a passive plasma wave instrument. RPI was a highly flexible instrument capable of being programmed to perform these types of measurements at times when IMAGE was located in key regions of the magnetosphere. For the remote sensing, RPI transmitted coded electromagnetic waves and used digital pulse compression and spectral integration to isolate the resulting echoes.
The RPI instrument consisted of an electronics unit, four 250-m wire antennas with antenna tuners, and a z-axis antenna with two 10-m lattice booms. RPI used the x axis antennas for all transmissions while echo reception was accomplished on all three. The x-axis dipole antenna was 500 m tip-to-tip at the beginning of the mission but was shortened to 370 m when it apparently collided with a micrometeoroid or orbital debris on 03 October 2000. The Y antenna suffered similar damage to its -Y segment 11 on August 2002 and complete loss of its +Y segment on 30 September 2004.
RPI was capable of detecting direct echoes from the plasmasphere from distances of 3 Earth radii or greater. RPI observed a large number of guided echoes in the plasmapause, plasmaspheric notches, in the plasma trough, and over the polar cap. These observations indicated that electromagnetic waves propagate along the magnetic field lines, often from one hemisphere to the other, possibly supported by field-aligned density structures. Inversion of RPI echo traces, guided or direct, provided a means of measuring evolving electron density distributions under a variety of geomagnetic conditions including plasmasphere depletion and refilling during a magnetic storm. RPI passive measurements also showed that AKR source locations move with season and local time and, when compared to Polar spacecraft observations, the overall intensity of AKR is less during solar maximum than solar minimum.
Information about the Radio Plasma Imager (RPI) experiment on the IMAGE mission.
IMAGE RPI Instrument page maintained by NASA GSFC with RPI facts, description, team, data, documents, discoveries, and related links sections
IMAGE RPI Instrument page maintained by University of Massachusetts Lowell with RPI description, team, software downloads, software user guides, access to CORPRAL automated prospecting results, mission planning tools and commanding guide, data model descriptions for Level 0 and 1, sonification files of 2003 Halloween storm, and useful links
| Role | Person | |
|---|---|---|
| 1. | Principal investigator | Prof. Bodo W. Reinisch |
| 2. | Data producer Technical contact |
Dr. Ivan A. Galkin |
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IMAGE (Imager for Magnetopause-to-Aurora Global Exploration) was a MIDEX class mission, selected by NASA in 1996, to study the global response of the Earth's magnetosphere to changes in the solar wind. IMAGE was launched March 25, 2000 into a highly elliptical polar orbit with initial geocentric apogee of 8.2 Earth radii and perigee altitude of 1000 km. IMAGE used neutral atom, ultraviolet, and radio imaging techniques to: (a) identify the dominant mechanisms for injecting plasma into the magnetosphere on substorm and magnetic storm time scales; (b) determine the directly driven response of the magnetosphere to solar wind changes; and, (c) discover how and where magnetospheric plasmas are energized, transported, and subsequently lost during substorms and magnetic storms.
In order to fulfill its science goals, IMAGE utilized neutral atom, ultraviolet, and radio imaging techniques. A suite of three neutral atom imagers (NAI) provided energy- and composition-resolved images at energies from 10 eV to 200 keV with a time resolution of 300 seconds. Two ultraviolet imagers, covering wavelength ranges from 120-180 nm (FUV) and 30.4 nm (EUV), provided coverage in the far and extreme ultraviolet. The radio plasma imager (RPI) was a low-power radar which operated in the radio frequency bands which contain the plasma resonance frequencies characteristic of the Earth's magnetophere (3 kHz to 3 MHz).
On December 18, 2005, after 5.8 years of successful operations, IMAGE's telemetry signals were not received during a routine pass. Preliminary analysis indicated that IMAGE's solid state power controller (SSPC) on the 28V line from the power distribution unit (PDU) to the transponder is reading closed, but is actually open resulting in having no power to the transponder to get a command to the PDU to close it. The only thing that might close it would be a PDU power cycle. It is possible that the next mega-eclipse cycle in October 2007, may drain the battery and voltage enough to cause this to happen enabling IMAGE to be recovered. For more details on the legacy of the IMAGE mission see the NASA press release at
http://www.nasa.gov/home/hqnews/2006/jan/HQ_06030_IMAGE_quits.html
Information about the IMAGE mission
| Role | Person | |
|---|---|---|
| 1. | Principal investigator | Dr. James L. Burch |
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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 |