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-1 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. Each ionogram consists of a fixed-frequency and and a swept-frequency portion. The time resolution between ionograms is typically 29 seconds.
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-1.
Users please acknowledge the Coordinated Data Analysis Web (CDAWeb) at the NASA Goddard Space Flight Center, ISIS-1 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-1 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 in preparation.
Repository of ISIS-1 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-1 SFS instrument Principal Investigator J. H. Whitteker and ISIS Data-Restoration project lead Robert F. Benson.
The cadence is 17 or 29 s for ionograms that have a swept-frequency portion from 0.1 to 10.0 MHz and 0.1 to 20 MHz, respectively. NOTE: for ISIS2 the appropriate values are 14 and 22.5 s, for 0.1 to 10.0 MHz and 0.1 to 20 MHz ionograms, respectively.
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
pulse per second code: 0= 30 pps, 1= 60 pps
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
fixed frequency code: 0=off, 1=0.25, 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
SEA instrument on(1)/off(0) status
IMS1 instrument on(1)/off(0) status
IMS2 instrument on(1)/off(0) status
SPS instrument on(1)/off(0) status
EPD instrument on(1)/off(0) status
scan line number of start of swept-frequency portion of the ionogram - seperates 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-1 binary ionogram files, one designated as "full" and one as "average". The full file has 1340 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 335 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 sounder receiver linear video amplitude, from 0 to 255 telemetry units, in each apparent-range bin of each scan line covering the fixed- and swept-frequency regions. This range corresponds to a linear sounder-receiver video amplitude output range from zero to 4.5 V. This calibration is based on the video calibration pulse (of 3.0 V or 170 telemetry units) at the end of the line scan following each sounder pulse (the combined calibration pulses from all of the line scans produces a colored stripe at the bottom of the digital ionograms). In order to derive an input power level corresponding to the receiver video output it is necessary to know the sounder-receiver automatic-gain-control (AGC) voltage. This voltage was obtained from the pcm data and thus is only available if pcm data were available. The AGC voltage, which ranges from 0 to 5.12 volts, is obtained from a linear interpolation between the AGC trace displayed between 4005 km apparent range (26.7 ms delay time) as 5.12 V and 4395 km (29.3 ms delay time) as 0 volts. (On the full ionograms these numbers are 4001.250 km or 26.675 ms, and 4398.750 km or 29.325 ms.) On the average ionograms, which are available as either CDF or binary files from the SPDF or the NSSDC, the range resolution is 0.1 ms (corresponding to a virtual-range resolution of 15 km) there are 27 rows (26 intervals) covering the 0 to 5.12 V range; thus each row in virtual range above (decreasing delay time) the zero level (at 29.3 ms delay time) corresponds to an increase of 5.12/26 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. (On the full ionograms, which are only 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
SPASE version 2.2.0
The ISIS 1 (International Satellites for Ionospheric Studies) Swept-Frequency Sounder measured the ionospheric electron density in the altitude range 300 to 3500 km, and provided correlative data for the other ISIS 1 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 19 or 29 s, and one of six selected frequencies was also used for sounding for a few seconds during each 19- or 29-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 Sweep-Frequency Sounder on ISIS 1
| Role | Person | |
|---|---|---|
| 1. | Principal investigator | Dr. J. H. Whitteker |
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ISIS 1 was an ionospheric observatory instrumented with sweep- and fixed-frequency ionosondes, a VLF receiver, energetic and soft particle detectors, an ion mass spectrometer, an electrostatic probe, an electrostatic analyzer, a beacon transmitter, and a cosmic noise experiment. The sounder used two dipole antennas (73 and 18.7 m long). The satellite was spin-stabilized at about 2.9 rpm after antenna deployment. Some control was exercised over the spin rate and attitude by using magnetically induced torques to change the spin rate and to precess the spin axis. A tape recorder with 1-h capacity was included on the satellite. The satellite could be programmed to take recorded observations for four different time periods for each full recording period. The recorder data were dumped only at Ottawa. For non-tape-recorded observations, data for the satellite and subsatellite regions could be acquired and telemetered when the spacecraft was in the line of sight of telemetry stations. The selected telemetry stations were in areas that provided primary data coverage near the 80-deg-W meridian and in areas near Hawaii, Singapore, Australia, the UK, 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 1 operations were terminated in Canada on March 9, 1984. The Radio Research Laboratories (Tokyo, Japan) then requested and received permission to reactivate ISIS 1. Regular ISIS 1 operations were started from Kashima, Japan, in early August 1984. ISIS 1 was deactivated effective January 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 1 mission
| 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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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 |