OrbitLink Duo VU1K2 transceiver

PRODUCT

OrbitLink Duo VU1K2 transceiver

Product Description

The Orbitlink Duo is a TRL-9 certified VHF APRS and UHF telecommand (TT&C) transponder system designed for CubeSats and small satellites. It handles critical telemetry and telecommand operations. Designed with low power consumption in mind, it ensures the efficient use of resources in space. Furthermore, the payload has undergone Environmental Stress Screening (ESS) testing, demonstrating robust performance under various environmental conditions.

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ProductDetail
Specification

Key Features

  • Receives and transmits data at 1.2k baud rate.
  • Accepts GPS signals for satellite tracking (optional).
  • Power Supply: Independent 5V system.
  • UART Interface: Independent interface.

Environmental Testing

The CubeSat payload has undergone Environmental Stress Screening (ESS) testing and has demonstrated robust performance under various environmental conditions.

Low Power Consumption

The CubeSat payload has been designed with low power consumption in mind, ensuring efficient use of resources in space.




 

Power Consumption

    5V 1A DC power is the minimum requirement.

General Specification

Input DC Power 5V, 3.5W Max on each band
Sleep Mode 15 mW
RX 300 mW in Receive mode
TX 1.9 ~ 3.8 W
Connectors SMA-Female
Operating Temperature -20ºC to +70ºC
Receive Sensitivity
  • VHF: -120 dBm
  • UHF: -115 dBm
Operating Frequency
  • VHF: 137 ~ 170 MHz (Specific Range)
  • UHF: 400 ~ 470 MHz (Specific Range)
RF Output Power 27 ~ 30 dBm
Modulation & Data Protocol AX.25 AFSK 1200 bps
GNSS Support Refer to CosmoOrbit XE specification.
Onboard Sensor Dual Temperature Sensor
Data Interface UART 9600bps for each band
Antenna Dual band dipole or monopole (optional)
 
 
ProductDetail

Key Features

  • Receives and transmits data at 1.2k baud rate.
  • Accepts GPS signals for satellite tracking (optional).
  • Power Supply: Independent 5V system.
  • UART Interface: Independent interface.

Environmental Testing

The CubeSat payload has undergone Environmental Stress Screening (ESS) testing and has demonstrated robust performance under various environmental conditions.

Low Power Consumption

The CubeSat payload has been designed with low power consumption in mind, ensuring efficient use of resources in space.




 
Specification

Power Consumption

    5V 1A DC power is the minimum requirement.

General Specification

Input DC Power 5V, 3.5W Max on each band
Sleep Mode 15 mW
RX 300 mW in Receive mode
TX 1.9 ~ 3.8 W
Connectors SMA-Female
Operating Temperature -20ºC to +70ºC
Receive Sensitivity
  • VHF: -120 dBm
  • UHF: -115 dBm
Operating Frequency
  • VHF: 137 ~ 170 MHz (Specific Range)
  • UHF: 400 ~ 470 MHz (Specific Range)
RF Output Power 27 ~ 30 dBm
Modulation & Data Protocol AX.25 AFSK 1200 bps
GNSS Support Refer to CosmoOrbit XE specification.
Onboard Sensor Dual Temperature Sensor
Data Interface UART 9600bps for each band
Antenna Dual band dipole or monopole (optional)
 
 
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