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.

Guidance system combining inertial navigation (self-contained motion tracking) with GPS (satellite-based positioning) for precise trajectory correction in ballistic missiles.

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.

Relating to or using nuclear energy, typically fission, for propulsion or power generation in military vessels.

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