Other features: The propulsion system is hybrid, featuring a solid-propellant rocket booster for launch and a turbofan engine (such as modified Ivchenko AI-25 variants) for sustained flight. The guidance suite combines GNSS/GPS navigation – supported by anti-jamming CRPA antenna arrays – with an inertial navigation system (INS), alongside open-architecture autopilot elements including integrated solutions from Safran and platforms like ArduPilot. The missile achieves high precision with a circular error probable (CEP) of approximately 14 meters.
