The telemetry systems ensure data gathering and transmission; the systems operate as part of launch vehicles, satellite platforms, orbital stations and ground segment.
The on-board computers ensure management and control of operation of non-hermetic long-lifetime spacecraft.
The communication equipment ensures reception and transmission of data for communication between the ground segment and the functional (onboard) system of a launcher, spacecraft or orbital station.
The video-telemetry system captures video of on-board equipment and transmits the video data in the form of TM signals via an in-built transmitter.
Visual monitoring system for spacecraft is intended for visual monitoring of solar cells panels deployment process and for thermal monitoring of spacecraft subsystems.
The navigation equipment defines position, altitude, speed and time by signals of GLONASS, GPS, GALILEO, QZSS, SBAS (WAAS, EGNOS, GAGAN) of L1 band as part of control systems of highly dynamic objects.
