This page summarizes information about the selected resource and its origin based on SPASE metadata.
SPASE version 2.2.1
These ionograms were digitized from the original ISIS-2 7-track analog telemetry tapes using the facilities of the former Data Evaluation Laboratory at the NASA/GSFC. This data restoration project is headed by Dr. R.F. Benson (NASA/GSFC). Ionograms were digitized at the rate of 40,000 16-bit samples/sec. This sample rate is higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 kHz provides a measurement every 25 microseconds corresponding to an apparent range (c*t/2) interval of 3.75 km. Ionograms with this sample rate are designated as "full" ionograms because they have the full 3.75 km apparent-range resolution. The ionograms used for most analysis, and those available from CDAWeb, were produced by averaging every four samples of the sounder-receiver video amplitude output to yield an average value every 100 microseconds corresponding to an apparent-range resolution of 15 km. These ionogram files are referred to as "average" files with standard resolution. Each ionogram consists of a fixed-frequency and and a swept-frequency portion. The time resolution between ionograms is typically 14 or 22 seconds depending on the frequency sweep range.
ISIS/Alouette page maintained by NASA GSFC with science and instrument descriptions, data access, software, and publication lists
Information about the Sweep Frequency Sounder experiment on ISIS-2.
Users please acknowledge the Coordinated Data Analysis Web (CDAWeb) at the NASA Goddard Space Flight Center, ISIS-2 SFS instrument Principal Investigator J. H. Whitteker and ISIS Data-Restoration project lead Robert F. Benson.
| Role | Person | |
|---|---|---|
| 1. | Principal investigator | Dr. J. H. Whitteker |
| 2. | General contact | Dr. Robert F. Benson |
| 3. | General contact | Dieter K. Bilitza |
FTP access to repository of ISIS-2 Ionograms in CDF format at NASA CDAWeb. The CDF files are organized by ground station, where each ground station is represented by a three letter ID and a two-digit code. The full names for each station are provided at http://nssdc.gsfc.nasa.gov/space/isis/isis-table1-new.html A merged data set, independent of the ground stations, is planned.
Repository of ISIS-2 data in CDF format at NASA CDAWeb, accessible via web interface.
Users please acknowledge the Coordinated Data Analysis Web (CDAWeb) at the NASA Goddard Space Flight Center, ISIS-2 SFS instrument Principal Investigator J. H. Whitteker and ISIS Data-Restoration project lead Robert F. Benson.
Note: The cadence is 14 or 22.5 s for ionograms that have a swept-frequency portion from 0.1 to 10.0 MHz and 0.1 to 20 MHz, respectively.
See discussion on "How To Detect Erroneous ISIS-2 Digital Ionogram Files" at http://nssdc.gsfc.nasa.gov/space/isis/isis_read_error.html
sat.-ID: 1=AL1, 2=AL2, 3=ISIS1, 4=ISIS2
two-digit telemetry station code
trans. power code: 1=Prim(400W) 2=Sec(400W)
sounder/receiver code: 0=off, 1=on
swept-f range code: 0=normal (swept-frequency from 0.1 to 10.0 MHz), 1=extended (swept-frequency from 0.1 to 20.0 MHz)
DMODE (transm. on/off for alternate frame pairs): 0=off, 1=on
GMODE (transmission of alternate frames of fixed-frequency ionograms and normal combined fixed- and swept-frequency ionograms): 0=off, 1=on"
sounder mixed mode (transmission at a fixed-frequency while the sounder receiver sweeps over swept-frequency range): 0=off, 1=on
AIT mode (automatic sounder operation every 3 min): 0=off, 1=on
fixed frequency code: 0=off, 1=0.12, 2=0.48, 3=1.00, 4=1.95, 5=4.00, 6=9.303 MHz
Year of ionogram frame sync in UT
Day of Year of ionogram frame sync in UT
Hour of ionogram frame sync in UT
Minute of hour of ionogram frame sync in UT
Second of minute of ionogram frame sync in UT
Local Mean Time (hh,mm) at time of ionogram frame sync
| Index | Name | Units |
|---|---|---|
| 1 | LMT(hh) | hrs |
| 2 | LMT(mm) | min |
geographic coordinates (Lat,Long,Hgt) at time of ionogram frame sync
| Index | Name | Units |
|---|---|---|
| 1 | latitude | deg |
| 2 | longitude | deg |
| 3 | height | km |
Geomagnetic Local Time (HHMM) at time of ionogram frame sync
| Index | Name |
|---|---|
| 1 | GMLMT(hh) |
| 2 | GMLMT(mm) |
geomagnetic latitude at time of ionogram frame sync
geomagnetic longitude at time of ionogram frame sync
invariant latitude at time of ionogram frame sync
Dip angle of mag field direction at time of ionogram frame sync
Solar Zenith Angle at time of ionogram frame sync
L shell (McIlwain parameter) at time of ionogram frame sync
spacecraft in(=1)/out(=2) sunlight at time of ionogram frame sync
CEP instrument on(1)/off(0) status
VLF receiver on(1)/off(0) status
RPA instrument on(1)/off(0) status
IMS instrument on(1)/off(0) status
SPS instrument on(1)/off(0) status
EPD instrument on(1)/off(0) status
RLP instrument on(1)/off(0) status
ASP instrument on(1)/off(0) status
scan line number of start of swept-frequency portion of the ionogram - separates the fixed- and swept-frequency portions
msec after frame sync - time of frequency markers
ionogram frequency markers
each sounder-pulse transmission is followed by a scan of the sounder-receiver video amplitude output values for each delay time monitored after the transmitted pulse; these scans are called scan lines. There are two types of ISIS-2 binary ionogram files, one designated as "full" and one as "average". The full file has 892 delay times (one every 0.025ms). The average files are derived from the full files by averaging the amplitude values in 4 delay-time bins. Thus the average binary files contain 223 time-delay bins within each scan line. The cdf files were made from these average binary files.
Ionogram files can be of different length. In some the swept-frequency portion covers the range 0.1 - 10 MHz, in others 0.1 - 20 MHz. Also, the proper start of each ionogram file, marked by a frame-sync pulse, was not always detected during the analog-to-digital (A/D) conversion. In such cases a frame sync was inserted to limit the file size. Thus the number of sounder-receiver video amplitude vs. delay time scan lines per ionogram can vary.
delay-time values used in each scan line
apparent-range values used in each scan line
The color scale represents a linear sounder-receiver video amplitude output range from zero to 4.5 V expressed in terms of telemetry units from zero to 255. This calibration is based on the video calibration levels at the end of the listening period following each sounder pulse (these calibration levels produce the multi-colored stripe at the bottom of the digital ionograms). The sounder-receiver automatic-gain-control (AGC) voltage (from 0 to 5.12 volts) is obtained from a linear interpolation between the AGC trace displayed between 2400 km virtual range (16.0 ms) as 5.12 V and either 2805 km (18.7 ms) on the average ionograms or 2801.25 km (18.675 ms) on the full ionograms2805 km (18.7 ms) as 0 volts. On the average ionograms, which are available as either CDF or binary files from the NSSDC, the range resolution is 0.1 ms (corresponding to a virtual-range resolution of 15 km) there are 28 rows (27 intervals) covering the 0 to 5.12 V range; thus each row in virtual range above (decreasing delay time) the zero level (at 18.7 ms delay time) corresponds to an increase of 5.12/27 V of AGC with a quantization uncertainty of approximately plus or minus 0.1 V. Two rows have zero video-output amplitude values (on the average ionograms) in order that a clear AGC trace is visible on the ionograms. The row with the greatest virtual range corresponds to the actual AGC value. These AGC values were obtained from the pcm data corresponding to the ionogram of interest; these pcm files are available from the NSSDC. If the ionogram analysis program (also available from the NSSDC) is used, the AGC voltage corresponding to the scaling of each X- and O-mode trace point is given as part of the output file with the extension .tra. On the full ionograms, which are available as binary files from the NSSDC, the range resolution is 0.025 ms (corresponding to a virtual-range resolution of 3.75 km) and three rows have zero video-output amplitude values; the middle row corresponds to the actual AGC value.
frequency of each scan line; in the swept-frequency portion of the ionogram they correspond to interpolated values between the frequency markers
Electron Gyrofrequency at time of ionogram frame sync
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The ISIS 2 (International Satellites for Ionospheric Studies) Swept-Frequency Sounder measured the ionospheric electron density in the altitude range 300 to 1400 km, and provided correlative data for the other ISIS 2 experiments, particularly those measuring ionospheric parameters. The ionosonde was a radio transmitter that recorded the time delay between a transmitted and returned radio-frequency pulse. A continuum of frequencies between 0.1 and 20 MHz was sampled every 14 or 21 s, and one of six selected frequencies was also used for sounding for a few seconds during each 14- or 21-s period. In addition to the sweep- and fixed-frequency modes of operation, a mixed mode was available in which the transmitter frequency was fixed at one of six possible frequencies while the receiver swept. Several virtual-range (delay-time) traces resulting from ground reflections, plasma resonances, birefringence of the ionosphere, nonvertical propagation, etc., were normally observed.
Information about the Swept-Frequency Sounder on ISIS 2
| Role | Person | |
|---|---|---|
| 1. | Principal investigator | Dr. J. H. Whitteker |
SPASE version 2.2.0
ISIS 2 was an ionospheric observatory instrumented with a sweep- and a fixed-frequency ionosonde, a VLF receiver, energetic and soft particle detectors, an ion mass spectrometer, an electrostatic probe, a retarding potential analyzer, a beacon transmitter, a cosmic noise experiment, and two photometers. Two long crossed-dipole antennas (73 and 18.7 m) were used for the sounding, VLF, and cosmic noise experiments. The spacecraft was spin-stabilized to about 2 rpm after antenna deployment. There were two basic orientation modes for the spacecraft, cartwheel and orbit-aligned. The spacecraft operated approximately the same length of time in each mode, remaining in one mode typically 3 to 5 months. The cartwheel mode with the axis perpendicular to the orbit plane was made available to provide ram and wake data for some experiments for each spin period, rather than for each orbit period. Attitude and spin information was obtained from a three-axis magnetometer and a sun sensor. Control of attitude and spin was possible by means of magnetic torquing. The experiment package also included a programmable tape recorder with a 1-h capacity. For nonrecorded observations, data from satellite and subsatellite regions were telemetered when the spacecraft was in the line of sight of a telemetry station. Telemetry stations were located so that primary data coverage was near the 80-deg-W meridian and near Hawaii, Singapore, Australia, England, France, Norway, India, Japan, Antarctica, New Zealand, and Central Africa. NASA support of the ISIS project was terminated on October 1, 1979. A significant amount of experimental data, however, was acquired after this date by the Canadian project team. ISIS 2 operations were terminated in Canada on March 9, 1984. The Radio Research Laboratories (Tokyo, Japan) then requested and received permission to reactivate ISIS 2. Regular ISIS 2 operations were started from Kashima, Japan, in early August 1984. ISIS 2 was deactivated effective 24, 1990. A data restoration effort began in the late ninties and successfully saved a considerable portion of the high-resolution data before the telemetry tapes were discarted. More information about this effort and access to the data on CDAWeb and nssdcftp can be found at
http://nssdc.gsfc.nasa.gov/space/isis/isis-status.html
Information about the ISIS 2 mission
| Role | Person | |
|---|---|---|
| 1. | Project scientist | Mr. John E. Jackson |
| 2. | Team leader | Mr. Larry H. Brace |
| 3. | Project scientist | Dr. Theodore R. Hartz |
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ISIS ionospheric observatories
| Role | Person | |
|---|---|---|
| 1. | Project scientist | Dr. Irvine Paghis |
| 2. | Project scientist | Mr. John E. Jackson |
| 3. | Team leader | Mr. Larry H. Brace |
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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 |