This page summarizes information about the selected resource and its origin based on SPASE metadata.
SPASE version 2.2.0
Collection of RPI Daily Dynamic Spectrogram plots at NASA GSFC, covering complete mission period from 2000-04-21 to 2005-12-18. Dynamic Spectrograms present the time history of natural radio emissions in space between 3 and 1009 kHz while the IMAGE spacecraft orbits the Earth. This operating frequency range was selected by the RPI team to provide an optimal temporal resolution to the wave observations. Each image is a daily plot of the voltage spectral density of received signal (color scale) as function of operating frequency (vertical axis) and time (horizontal axis). 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. RPI Dynamic Spectograms plot a Voltage Spectral Density, which is root of power spectral density, measured in [V/root-Hz] units. Note that conversion of antenna voltage to electric field strength depends on effective length of receive antennas, and such conversion is not performed here. 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.
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
Users please acknowledge B. W. Reinisch of the University of Massachusetts Lowell and J. L. Green of the NASA Goddard Space Flight Center for making these dynamic spectrograms available.
| Role | Person | |
|---|---|---|
| 1. | Principal investigator | Prof. Bodo W. Reinisch |
| 2. | Data producer Technical contact |
Dr. Ivan A. Galkin |
Repository of RPI dynamic spectrogram images at NASA GSFC, containing web interface to individual images.
Users please acknowledge B. W. Reinisch of the University of Massachusetts Lowell and J. L. Green of the NASA Goddard Space Flight Center for making these dynamic spectrograms available.
In Cadence below, the 5 minutes refers to the nominal interval between measurements used to make up a 24-hour dynamic spectrogram. The cadence can be as small as 3 minutes, 5 minutes is a typical value. Display Cadence (further below) refers to the 24-hour interval between the start of two successive dynamic spectrograms.
(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 interfererence 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). The RPI instrument noise floor is 5 nV/root-Hz = -166 dB(V/root-Hz) at the receiver input.
SPASE version 2.0.0
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 |
SPASE version 2.2.0
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 |
SPASE version 2.2.0
SPASE version 2.2.0
SPASE version 2.2.0
SPASE version 2.2.0