TM/TC Front-End
CELESTIA Satellite Test & Simulation
Telemetry and telecommand unit for direct spacecraft control during AIT and launch phases — 60x RS422/LVDS pairs, galvanically isolated.
Technical specifications
- Form factor
- 19" 3U hardware platform
- Baseband interfaces
- 60x RS422/LVDS pairs
- Isolation
- Galvanically isolated, FMEA compliant
About
A telemetry (TM) and telecommand (TC) unit which provides direct control of spacecraft using baseband interfaces during spacecraft development, assembly, integration, test (AIT) and launch phases. Used for spacecraft onboard computer testing, flight transponder testing, or communication with the spacecraft before launch, typically connecting to the spacecraft OBC or CDMU via direct bypass interfaces or via an RF SCOE.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
