SMU is a robust, reliable and powerful flight computer compatible with different space orbits. Because of high reliable LEON3 processor architecture and modular structure of SMU it can be adapted to different space platform needs.
SMU provides the following features to the satellite flight segment:

Supply 28V nominal (15V to 50V input voltage range)
Power: 38W (nominal)
Dimension: 293 mm x 279 mm x 294 mm (W x L x H)
Weight 12.7kg
2 x 3 TC Input (RS-422), 2 x 3 TM Output (RS-422)
4 + 4 System Alarm (RS-422)
2 x 2 MIL-STD-1553 2 x 4 CAN
2 x 2 UART (RS-422)
2 x 1 JTAG
Synchronization :
2 x 2 PPS In (RS-422)
2 x 6 Sync Out (RS-422)
HV-HPC 2 x 16
LPC 2 x 10
ASM 2 x 18
TSM1 2 x 128
TSM2 2 x 33
BSM/BDM 2 x 16
IMECE, TURKSAT 6A, AYAP-1
Thermal:-20 to +50 C
Vibration
Shock
EMI/EMC: MIL-STD-461
Lifetime: 5 to 15 years
SEU tolerant
Latchup Immune