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 where a missile receives mid-flight course corrections from an external source, such as ground control or satellite.

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.

A two-stage ATGM propulsion system where a booster stage initially accelerates the missile before a sustainer stage maintains flight velocity.