Guidance system using onboard radar to actively emit and receive signals for target tracking and missile course correction.

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

A proximity fuze is a detonation mechanism in ATGMs that triggers when the missile approaches within a set distance of a target, using sensors like radar or laser to detect proximity.

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