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.

Launched from a ground-based platform, such as a vehicle or tripod, rather than an aircraft or other airborne system.

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

Missile guidance system where commands are transmitted via a physical wire link between the launch point and the missile during flight.