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 Satellite Detail - Weber-OSCAR 39
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Photo of Weber-OSCAR 39

Weber-OSCAR 39
(JAWSAT )


Spacecraft Summary

OSCAR Designation:  Weber-OSCAR 39     Oscar Number:  WO-39    
International Designator:  2000-004A     Norad Number:  26061    
Common Name:  JAWSAT     Satellite Type:  Microsatellite    
Launch Date:  27 January, 2000     Launch Location:  AFWTR    
Launch Vehicle:  Minotaur-1     Apogee:  788.00    
Perigee:  738.00     Inclination:  100.19    
Period:  100.10     Weight:  0.000 Kg    
Organization: Weber State University


Frequency Information
 
Mode V/U (J) Packet: Non-Operational
Uplink: 145.8600 MHz FSK 9600 BPS
Downlink 437.4000 MHz FSK 9600 BPS
 
Mode S TLM Beacon: Non-Operational
Downlink 2403.2000 MHz FSK 9600 BPS


Detailed Description

JAWSAT stands for Joint Air Force Weber Satellite which was a joint project between the U.S. Air Force and Weber State University.

Launched January 27, 2000 from Vandenburg AFB in California.

JAWSAT served as a bus for several deployable payloads and the Plasma Experiment Satellite Test experiment -- called PEST. The telemetry stream from JAWSAT, including data from the PEST project, was to be transmitted on Amateur Radio frequencies.


Reference Documents:

  • Axelrad, P. and B.C. Chesley, "Performance Testing of a GPS Based Attitude Determination System.," AIAA Guidance, Navigation, and Control Conference, Monterey, CA, 809-819, August 1993. (Received award for best paper presented at the conference.)
  • Chesley, B.C. and P. Axelrad, "An Integrated GPS Attitude Determination System for JAWSAT," ION-GPS 94, Salt Lake City, 1251-1261, September 1994.
  • Chesley, B.C. and P. Axelrad, "Mitigating Measurement Errors in a Low Cost Satellite Attitude Determination System," ION National Technical Meeting, Anaheim, CA, 763-774, January 1995.
  • Chesley, B.C. "An Integrated GPS Attitude Determination System for Small Satellites," Ph.D. Dissertation, University of Colorado, July 1995.

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