Flight Termination System is a fully redundant range safety and test system.
Flight Termination System is a fully redundant range safety and test system. Main function of the FTS is to send commands to the flight termination receivers on board when necessary.
System is composed of redundant command consoles, signal generators, power amplifiers, antenna switching unit and antennas. The users can select in between redundant channels on the fly.
System Includes;
- 2 Control Panels
- 2 Power Supply Units
- 1 Control Unit
- 1 Antenna Switching Unit (8 antennas)
- Associated Cabling
Key Specifications
- Programmable RF center frequency
- Programmable tone frequencies
- 4 Tone Outputs
- Full Redundancy 2 RF Outputs, 2 Power Supply Units
- Antenna switching unit available for Various Antenna Options
- RF output fault detection
- Programming interface for monitor and control power output levels, switching RF outputs and antennas
- Output command verification
- Supports 20 IRIG Tones
- Easy and Safe Maintenance
- RCC 319-14 Compatible
| Power Consumption (w) | <750 W for 250W System |
| Frequency Range | 390 - 450 MHz |
| Operating Temperature | -40 °C to +85 °C |
| Max. RF Output Power | 100 W / 250 W / 500 W / 1000 W |
| Input Voltage | 180 - 264 VAC, 47-63 Hz |
| Tone Frequencies | 20 IRIG Tones |
| Connectors | N-Type |
| Programming Interface | RS232 |
| EMI / EMC | MIL-STD-461F |
