Capability of launching an anti-tank guided missile from an airborne platform, such as a helicopter or aircraft.

The initial propulsion phase where a high-thrust motor accelerates the missile to operational velocity.

A guidance system in ATGMs that uses infrared sensors to create a thermal image of the target for precise homing.

A guidance method that uses inertial navigation sensors together with satellite‑based GPS signals to determine a missile’s position and steer it toward a target.

Guidance system using television or electro-optical sensors to track targets via visual or infrared imagery for missile navigation.

Enables real-time sharing of position, targeting, and sensor data among aircraft and platforms for coordinated combat operations.