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.

Characterized by a flight speed exceeding Mach 5, or approximately 6,150 km/h (3,800 mph) or higher.

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

A guidance system that uses directed laser beams to track and adjust the trajectory of a missile toward its target.

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