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

Guidance method where a missile follows a directed energy beam (e.g., radar or laser) to its target.

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

A lightweight, shoulder-fired anti-tank guided missile system designed for individual soldier transport and operation.

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

A tandem warhead configuration in anti-tank missiles where a smaller precursor charge detonates reactive armor, followed by a larger main charge to penetrate the underlying armor.

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