The payload of CAS-1 will likely include a CW telemetry beacon, a linear transponder, an FM repeater and a digital store and forward transponder. These operations will use 2 meters for uplinks and 70
centimeters for downlinks at 500mW output power.
The satellite is expected to be launched from China into a sun synchronous orbit with a 670 km apogee. According to Chen the CAS-1 team is waiting for another payload to be finished before launch date is officially set.
[F5NZO]
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Last Updated (Sunday, 03 August 2008 13:19)












