S-band Transceiver
Price on request
• Operates in the 2200-2290 MHz and 2025-2110 MHz EESS/SRS/SOS allocation
• Full duplex operation
• CCSDS compliant channel downlink coding ensures compatibility with many off-the-shelf demodulators as well as
various ground station networks
• AX.25 / HDLC uplink implementation allows robust yet low-complexity telecommand link implementation
• Strong Forward Error Correction (FEC) to maximize link throughput
• No need for data pre-processing: all channel coding is performed inside the transceiver
• In-flight configurable downlink RF parameters (Frequency, data-rate, RF power, FEC parameters)
• Safety watchdog
• Transmit power control loop to keep RF output power constant over varying operating conditions
• IPC-A-610 Class 3 assembly
Description
The ISISPACE CubeSat compatible S-band Transceiver is comprised of two PCBs, designed to meet the needs of telemetry downlinks, high data-rate downlinks of up to 4.3 Mbps (usable information bit-rate at CCSDS transfer frame level) and telecommand uplinks of 9.6 kbps (AX.25). The S-band transmitter is flexible, implementing CCSDS as data link layer protocol and allowing in-flight configuration of data-rate, modulation scheme, frequency, and RF output power. The system is designed for full-duplex TT&C and Payload data downlink, a diplexer is used such that a single antenna can be used for uplink and downlink.
Specifications
Dimensions: | 99 x 94 x 15 mm (transmitter PCB) 96 x 92 x 10 mm (receiver PCB) |
Mass: | 132g (transmitter) + 85g (receiver) |
Supply voltage range: | 7 to 20 V |
Power consumption: | Transmit mode: 13 W (for 33 dBm RF output power) Receive-only mode: 1.2 W |
Operating temperature: | -40 to +70 °C |
RF interfaces: | SMPM connector, 50 Ohms |
Payload downlink data interfaces: | LVDS |
Housekeeping data & uplink telecommand interface | I²C |
Transmitter
Frequency range: | 2200 – 2290 MHz |
RF output power: | 27 to 33 dBm (settable) ± 1 dB typ. |
Transmitted data rate (on-air): | up to 10 Mbit/s (5 Msym/s, OQPSK) |
Modulation scheme: | Suppressed carrier: BPSK, OQPSK selectable as per CCSDS 401.0-B |
Forward Error Correction: | Convolutional (K=7, ½) as per CCSDS 131.0-B Reed Solomon (223, 255) as per CCSDS 131.0-B |
Pseudorandomization: | Pseudorandomization as per CCSDS 131.0-B |
Synchronization: | 32 bit Attached Sync Marker as per CCSDS 131.0-B |
Receiver
Frequency range: | 2025 – 2110 MHz |
Noise figure: | < 4 dB (measured at diplexer RF input / output port on TXS) |
Data rate (on-air): | 9.6 kbit/s |
Modulation: | FSK and GMSK, supported BT = 0.3 … 0.5 |
Forward Error Correction: | None |
Pseudorandomization: | Pseudorandomization using G3RUH scrambling polynomial |
Data link layer protocol: | AX.25 or HDLC |
Configuration
The following default RF parameters can be configured:
• Transmit frequency
• Receive frequency
• Modulation scheme
• Roll-off
• Symbol rate
• Transmit power
• CCSDS Spacecraft Identifier
• Data link layer protocol (AX.25 or HDLC)
• I²C watchdog implementation
• CSKB-lite connector configuration
• Grounding interface configuration
Qualification and Acceptance testing
Test | QT | AT |
Functional | ✓ | ✓ |
Vibration | ✓ | ‐ |
Mechanical Shock | ✓ | ‐ |
Thermal Cycling | ✓ | ✓ |
Thermal Vacuum | ✓ | ‐ |
*QT is performed on the design/qualification model
*AT is performed on the unit to be shipped