Satellite Core Avionics (SCA)
STI’s Satellite Core Avionics combines the Onboard Computer (OBC) and Power Control/Distribution Unit (PCDU) functions in one compact unit.
It is a powerful centralized solution for small, 3-axis controlled satellites.
Satellite Core Avionics engineering model
SCA key features
Based on the SCA architecture, essential resource saving and optimization leads to:
- A smart, compact and flexible design base on the cPCI-Serial-Space standard.
- Powerful, modular and highly integrated avionics solution for small /medium satellite platforms.
- SCA architecture open for a full set of AOCS actuators/sensors for 3-axis controlled satellite platforms.
|OBC functions distributed over the following PCBs:||
|PCDU functions distributed into the following PCBs:||