AMSAT - Amateur Satellite Summary - AMRAD-OSCAR-27
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fahnen/6.jpg Amateur Satellite Summary - AMRAD-OSCAR-27
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AMRAD-OSCAR 27


Satellite Summary

Name: AMRAD-OSCAR 27 aka EYESAT-1
NASA Catalog Number: 22825
Launched: September 26, 1993
Launch vehicle: Ariane 4
Launch location: Kourou, French Guiana
Weight: 11.8 kg
Orbit: Polar LEO (Low Earth Orbit)
Inclination: 98.5 degrees
Size: 150 x 150 x 150 mm
Period: 101 Minutes

Uplink:

  • 145.850 MHz
Downlink:
  • 436.795 MHz
Features:
  • Amateur payload combined with an experimental payload.
  • EYESAT-1 is an experimental Microsat satellite built by Interferometrics Inc, of Chantilly, Virginia.
  • The amateur equipment onboard the satellite was built by AMRAD.
  • For further information about AMRAD contact:
Status: Semi-Operational

Description

AMRAD/EYESAT-1 was one of six satellites that was launched together on a Ariane V59 rocket from French Guiana at approximately 0147 UTC, 26 September 1993. The amateur payload of EYESAT-1 was later designated AMRAD-OSCAR 27 once in orbit. The launch included the German Stella Laser Reflector, Healthsat-II, PoSAT-1, and amateur satellites KITSAT-OSCAR-25 (KO-25) and Italy-OSCAR-26 (IO-26).

AO-27 is a secondary amateur communications payload carried aboard the EYESAT-1 experimental MICROSAT satellite built by Interferometrics Inc. of Chantilly, Virginia.  The commercial side of the spacecraft's mission is the experimental monitoring of mobile industrial equipment.

The amateur equipment aboard the satellite was constructed by members of AMRAD, a technically oriented, non-profit organization of radio amateurs based in the Virginia suburbs of Washington, D.C., to meet the needs of amateurs for a platform to conduct digital satellite communications experiments.

AO-27 is an "FM Repeater" in space.  It essentially consists of a crystal controlled FM receiver operation at 145.850 MHz and a crystal controlled FM transmitter operating at approximately 436.795 MHz.  Output power of the transmitter can be set to over 1 watt (rarely used), 0.5 watts (normal operation), or under 0.1 watts (exciter only).  The uplink antenna is the linear polarized whip on the top face of the spacecraft and is shared with the commercial payload's receivers.  The downlink antenna is a 1/4 wave whip mounted on the bottom face of the spacecraft.  Polarization is nominally linear, the rotation and revolution of the spacecraft and propagation effects will cause the actual signal polarization at a ground station to vary widely during a pass.

Because of the satellite's limited power budget and a desire to maintain sufficient battery capacity for as many years as possible, the amateur transmitter on AO-27 is on for only part of the daylight portion of each orbit.  As of September 1998, the satellite passed its five year design goal with minimal signs of battery degradation, so this operating philosophy appears to have been successful.

AO-27 is available on daylight passes over the Northern Hemisphere.  The "TEPR" States describe the amount of time (in minutes) when the spacecraft enters and leaves sunlight.  TEPR numbers are adjusted every few months to account for the seasonal North/South movement of the latitudes where AO-27 enters and exits sunlight.  Chuck Wyrick, N1UC (formerly KM4NZ), provides an Explanation of TEPR States.  Most tracking programs will provide a reading or display the necessary info to predict if AO-27 will be "on" during a pass.

More information on AO-27's schedule and operation courtesy of Michael Wyrick, N4USI, the control operator of AO-27 and Steve Greene, KA1LM.

[Special thanks to Stephan Greene, KA1LM, for assisting in the above information -- N7HPR]


References

  • John Hansen, "New Satellites in Orbit," The AMSAT Journal, Vol. 16, No. 5, Sep/Oct 1993, p. 1.
  • Steve Ford, "AMRAD Oscar 27," QST, Dec 1993, p. 107.

Last update May 31, 2003 - N7HPR


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