The Flight Termination System (FTS) is a fully redundant turn-key range safety and test system for remote control and flight termination of airborne test vehicles. The FTS consists of SPC's Command Transmitter System (CTS) and custom control, interface, and monitoring subsystems. The system is fully programmable and is flexible enough to meet the changing requirements of today's modern test ranges.
The FTS control software features a LabVIEW-based graphical user interface (GUI) that can be easily customized to suit specific requirements. FTS software automatically coordinates communication and control among range-control subsystems, site-control subsystems, and CTS units. The user-friendly interface is simple and straightforward, yet provides considerable power and flexibility.
The FTS is generally deployed in one of two configurations listed below:
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