Flight Termination System (FTS)
PacSci EMC
Modular flight termination system for missiles, satellite launch rockets, and unmanned aircraft, configured and qualified to range and program requirements.
Technical specifications
- Redundancy
- 5 redundant ordnance events
- Interface
- Mission Computer via High Speed serial Bus
- Testing
- Built-in test for electronics and fiber optic connection quality
- Cabling
- Rugged fiber optic cables
- Compliance
- MIL-STD-1901A and RCC319 qualified
- Reliability
- >0.999 @ 95% confidence
- Design
- Open, modular, stackable, reconfigurable (OSMR)
- Options
- Linear and bulk charges with flight heritage
About
PacSci EMC’s Flight Termination System (FTS) is designed for missiles, satellite launch rockets, and unmanned aircraft. All FTS products are configured, tested and qualified to the requirements of the customer’s range and program, preventing accidental initiation while ensuring the system responds only when commanded. The system uses an open, modular, stackable, reconfigurable (OSMR) design with rugged fiber-optic cabling and built-in test capability for electronics and fiber optic connection quality.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
