The Space Qualified Processor Unit (MICROSATPRO) is a high-performance satellite mission computer (On-Board Computer) compatible with micro-satellite platforms.

MICROSATPRO is a control unit that is resistant to harsh space conditions, has high fault tolerance, is reliable and has high processing power. While LEO is targeted as its operating orbit, it is designed to remain in this orbit for at least five years.

MICROSATPRO has an operating system running on FPGA (soft processor based). It is supported by interfaces (RS485, RS422, CAN, Spacewire, SPI, I2C, etc.) that are frequently used in micro-satellite platforms. Thanks to its modular design, it can be easily integrated into the target platform.

For protection from Single Event Effects, Fault Tolerant (FT-LEON3) core for processor within MICROSATPRO, Triple Modular Redundancy (TMR) in FPGA, Error Detection and Correction (EDAC) in memory units, Watchdog on software, LCL (LCL) in power units. Latch-up Current Limiter) measures have been taken.