IARU Amateur Satellite Frequency Coordination

 
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Cepheus Updated: 13 May 2016   Responsible Operator Josť Manuel Quero Reboul
Supporting Organisation Department of Electronic Engineering  
Contact Person quero@us.es.nospam  
Headline Details: Cepheus mission is a 3U CubeSat mission for in-orbit technologies demonstration, with four different payloads: - A fuel cell with an Instrument Control Unit to study the behviour of this energy system in-orbit environment. - An experimental on-board transceiver in order to evaluate the communication link through it. This transceiver will work at the same frequency for uplink and downlink than the principal one, operating alternatively and never simultaneously. - A Star Tracker designed by MEMS Technologies. - An Attitude Dynamics and Control Software in order to evaluate the model and software in-flight. Proposing to use a BPSK 1k2/9k6 downlink on VHF using AX25. Planning a 600km SSO orbit in H1 2016.No further information has been received about this mission**
Application Date: 28 Oct 2014   Freq coordination completed on

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