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ISIS 2

NSSDCA/COSPAR ID: 1971-024A

Description

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 3-5 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 one hour capacity. For non-recorded 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 01 October1979.

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 09 March 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 January 1990. A data restoration effort began in the late 1990s and successfully saved a considerable portion of the high-resolution data before the telemetry tapes were discarded.

More information about this effort and access to the data on CDAWeb can be found at

http://nssdc.gsfc.nasa.gov/space/isis/isis-status.html

Alternate Names

  • International Sats for Ionosph Studies
  • ISIS-B
  • 05104

Facts in Brief

Launch Date: 1971-04-01
Launch Vehicle: Delta
Launch Site: Vandenberg AFB, United States
Mass: 264.0 kg

Funding Agencies

  • NASA-Office of Space Science Applications (United States)
  • Radio Research Lab (Japan)
  • Department of Communications/Communications Research Centre (Canada)

Disciplines

  • Astronomy
  • Earth Science
  • Space Physics

Additional Information

Questions or comments about this spacecraft can be directed to: Dr. Dieter K. Bilitza.

 

Personnel

NameRoleOriginal AffiliationE-mail
Dr. J. H. WhittekerGeneral ContactDepartment of Communications/Communications Research Centre 
Mr. Marius B. WeinrebProgram ManagerNASA Headquarters 
Dr. Nobuo MatuuraGeneral ContactRadio Research Laboratorymatuura@stelab.nagoya-u.ac.jp
Mr. E. D. NelsenProject ManagerNASA Goddard Space Flight Center 
Dr. Erwin R. SchmerlingProgram ScientistNASA Headquarters 
Mr. John E. JacksonProject ScientistNASA Goddard Space Flight Center 
Dr. Theodore R. HartzProgram ScientistDepartment of Communications/Communications Research Centre 
Mr. Larry H. BraceProject ManagerNASA Goddard Space Flight Center 
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