Communication Subsystem for Small Satellites
Communication subsystem for the payload data link of a small satellite (approx. 100 kg, low Earth orbit below 600 km, mission duration 3 years): includes an S-band receiver (uplink), an S-band transmitter (downlink), and an X-band transmitter (downlink), as one device or a combination of several devices. One flight model (FM) and two engineering models (EM) are to be procured. An additional X-band telecommand receiver is optionally requested.
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