FZ219 is a lightweight composite material high-drag, straight cylindrical 12-tube reusable launcher designed for helicopter use. The FZ219 is equipped with removable universal dual purpose FZ125 detent mechanism enabling to fire FFAR and WA rockets.

The design of the FZ219 is identical to that of the rocket launcher FZ231, but without LIU interface (Launcher Interface Unit) equipped.

It can be fitted with an optional removable rear fairing.

Reference data

  • Document reference : STB M0219-30-0001-01 Technical requirements specification
  • NATO Stock Number (NSN) : 1055-13-118-4911

Mechanical characteristics

The FZ219 rocket launcher system includes a twelve (12) tube rocket composite central section.

  • Height : 316 mm
  • Width : 324 mm
  • Overall length : 1634.5 mm
  • Total mass (empty) : 29 kg


  • Firing mode : ripple / single
  • Intervallometry : 80 ms (minimum)
  • Dual purpose : designed for firing both types of FZ 2.75" FZ® FFAR and WA rocket motors
  • Rocket warheads : designed for firing all types of conventional 2.75" FZ® rocket warheads equipped with remote set fuze