SUBSYSTEMS

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Get to know our satellite subsystems

Our platforms employ in-house developed, powerful & robust subsystems for the success of your mission.

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STRUCTURES

3-12U Structures (STRU)

C3S offers two different designs when it comes to structures so that every customer can find the right solution. The one used during the Radcube mission has a stackable design along with unique wiring system, while the other design allows flexible payload and subsystem positioning for optimal configurability.

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EPS

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Electrical Power System (EPS)

Main Features

Flight heritage acquired in 2021 with the launch of RadCube
Cold Redundancy and Graceful Degradation
Single point failure tolerant
Telemetry and telecommand communication with redundant CAN bus
Temperature ranges:

circuits: -40°C to 80°C qualified
battery: 0°C to 50°C

Autonomous LCL protection
Autonomous Battery heater and balancing
Two-level battery undervoltage protection
Robust aluminium (T-7070) milling case
Radiation tested (TID)

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OBC

On-Board Computer (OBC)

Main Features

Flight heritage acquired in 2021 with the launch of RadCube
Single-point failure tolerant design
Cold redundancy
High-performance MCU
Optional Daughterboard for memory expansion
Serial communication interfaces using differential signaling (CAN, M-LVDS)
Computing performance: up to 642 DMIPS
Space grade connector to the backplane
ESA approved Interface Control Document
Radiation tested (TID)

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CHP-OBC

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Customizable High-Performance OBC

The CHP-OBC is a general-purpose computation platform for nano- and microsatellites. It provides high computation capacity, versatile and flexible interface capabilities, and robust and reliable power supply for payload subsystems.