Modern devices for space research are impossible to imagine without devices that don`t use the digital data
processing methods and specialized or standard interfaces and computing facilities. There are several approaches to
implement this trend: the use of standard devices and components, development and use of application-specific
integrated circuit (ASIC) and the creation of specialized units based on programmable logic integrated schemes
(PLIS). Obviously, the use of standard components in comparison with PLIS and ASIC, has major flaws - notably
the large size, weight and power consumption. In addition, it looks problematic the requirements of reliability (due
to excess of functions and/or hardware interfaces) and radiation hardness or tolerance (RH/RT).