Bus Tester development kit c3s - SmallSat Catalog - Orbital Transports
Additional Information
Voltage output:
12 V unregualted
Voltage output:
5 V
Voltage output:
3.3 V
Interface:
CAN
Interface:
UART
Interface:
SPI
Interface:
LVDS
Interface:
Ethernet
Dimensions:
86 x 171 mm
Documentation

C3S offers payload providers a development kit as a support during the whole integration process. Our hardwarein-the-loop bus tester is capable of testing the internal communication protocols of the satellite, making it possible to simulate real space usage by sending commands and verifying the correctness of the received data before flight. Thus, eliminating risks and making payload integration process smoother along with the verification of the electrical and software compliance of the ICD.

Main Features:

  • Tests can be executed during the development flow
  • Test processes are performed in the cloud providing traceable test results
  • Guaranteed real-time connection
  • The protection of the unit under test is provided by a three configurable limiter switch, monitoring the supply power
  • Customization and configuration of the device can be performed according to customer needs

Bus Tester C3S

C3S Electronics Development
Description

C3S offers payload providers a development kit as a support during the whole integration process. Our hardwarein-the-loop bus tester is capable of testing the internal communication protocols of the satellite, making it possible to simulate real space usage by sending commands and verifying the correctness of the received data before flight. Thus, eliminating risks and making payload integration process smoother along with the verification of the electrical and software compliance of the ICD.

Main Features:

  • Tests can be executed during the development flow
  • Test processes are performed in the cloud providing traceable test results
  • Guaranteed real-time connection
  • The protection of the unit under test is provided by a three configurable limiter switch, monitoring the supply power
  • Customization and configuration of the device can be performed according to customer needs
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Additional Information
Voltage output:
12 V unregualted
Voltage output:
5 V
Voltage output:
3.3 V
Interface:
CAN
Interface:
UART
Interface:
SPI
Interface:
LVDS
Interface:
Ethernet
Dimensions:
86 x 171 mm
Documentation

C3S offers payload providers a development kit as a support during the whole integration process. Our hardwarein-the-loop bus tester is capable of testing the internal communication protocols of the satellite, making it possible to simulate real space usage by sending commands and verifying the correctness of the received data before flight. Thus, eliminating risks and making payload integration process smoother along with the verification of the electrical and software compliance of the ICD.

Main Features:

  • Tests can be executed during the development flow
  • Test processes are performed in the cloud providing traceable test results
  • Guaranteed real-time connection
  • The protection of the unit under test is provided by a three configurable limiter switch, monitoring the supply power
  • Customization and configuration of the device can be performed according to customer needs