On-Board Interfaces
A satellite interface consists of various subsystems, such as Power, Communications, Data Handling, Onboard Computer, etc. All these sub-systems use a wide variety of satellite interfaces, both internally (within a sub-system) and externally (between sub-systems). These On-Board Interfaces can differ at many levels, such as physical, electrical and on protocol level. To support (sub-)system manufacturers during development and validation phases, C-STS offers a wide range of front-end products.
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Multi-Purpose Interface Platform
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TM/TC Front-End
The TM/TC Front-End is 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.
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WizardLink Front-End
The WizardLink Front-End provides high-speed serial interfaces to spacecraft flight equipment. WizardLink is used during spacecraft assembly, integration and test phase to test and validate satellite flight equipment.
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LVDS Front-End
The LVDS Front-End provides the Low-voltage differential signaling (LVDS) Data/Clock interfaces (electrical and protocol) to satellite flight equipment and can be used on all assembly, integration, and testing (AIT) levels (bread-boarding, module, unit, instrument, panel, and satellite).
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