HARDWARE / PRODUCTAdded 12 Jul 2026

S-Band Transceiver SRS-4

NanoAvionics
S-Band Transceiver SRS-4

High-speed full-duplex S-band transceiver for micro- and nano-satellites, up to 5 MBd TX, BPSK/QPSK/8PSK, CCSDS coding, 33 dBm output.

Typed specifications7 values

Discloses 2 of 13 fields engineers filter by in this category (category median 3).

Mass
253 g
product page
Frequency range
2 200–2 290 MHz
product page 2 025–2 110 MHz
Modulation
BPSK
product page QPSK  |  8PSK
Supply voltage
5.1–28.8 V
product page

Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.

As published by the supplier12 lines, in the manufacturer's own wording
Type
Full-duplex S-band high-speed transceiver
Transmit frequency
2200 to 2290 MHz
Receive frequency
2025 to 2110 MHz
Variable transmit symbol rate
Up to 5 MBd
Transmit modulation
BPSK, QPSK, 8PSK
Receive modulation
BPSK, QPSK (up to 5 MBd)
Transmit power
Adjustable 20 dBm to 33 dBm (with power monitoring)
Receive sensitivity
-122 dBm (<1% PER, 100 kBd BPSK)
Channel coding
CCSDS-recommended
Supply voltage
5.1 – 28.8 V
Mass
253 g
Interfaces
CAN-bus, RS-422 (CSP), Ethernet (IP)

About

The NanoAvionics SRS-4 is a full-duplex S-band transceiver designed for high-speed data transfer on micro- and nano-satellites. It operates on ITU space operations S-band frequencies (TX: 2200–2290 MHz, RX: 2025–2110 MHz) using BPSK, QPSK, and 8PSK modulation with CCSDS-recommended channel coding, enabling integration with both independent and commercial ground station networks.

The SRS-4 supports variable transmit symbol rates up to 5 MBd and receive rates up to 5 MBd, with adjustable output power up to 33 dBm and built-in power monitoring and regulation. CAN-bus and RS-422 interfaces (CubeSat Space Protocol) and an Ethernet interface with IP routing allow flexible integration into the satellite data handling architecture.

The unit weighs 253 g and accepts input voltage from 5.1 to 28.8 V, suitable for a wide range of CubeSat and SmallSat buses. Its high data rate capability makes it ideal for missions with large downlink requirements such as Earth observation or in-orbit experiments.

Documentation

No public datasheet yet — request the datasheet / ICD from the supplier.

Source: nanoavionics.com ↗

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