The AGM-65E missile has two major sections— the guidance and control section and the center/aft section. Four fixed wings are an integral part of the center/aft section, and four movable control surfaces (fins) are located at the aft section. These fins are installed or removed to aid in handling. The missile is issued to the fleet as an AUR. Installation of the fins is the only assembly required at the organizational maintenance level. The AGM-65E missile system has all the laser missile features, including automatic terminal homing on laser energy reflected from the target, which is illuminated by a laser designator. The laser designator can be a ground device, either hand-held or tripod mounted. It can also be a stabilized airborne device, mounted either on a separate aircraft or on the launching aircraft. Additionally, the warhead provides kinetic penetration into earth-barricaded or concrete fortifications and ships. The fuzing system allows a selectable detonation delay to optimize kill capability. For further information on the AGM-65E Maverick, you should refer to Laser-Guided Missile AGM-65E (Maverick), NAVAIR 11-120-58.