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.

Manual Command Line-of-Sight guidance; an ATGM control method where the operator manually steers the missile to the target using visual tracking.

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