AGM-65 Maverick

Developed during the Vietnam War as a subsonic, launch-and-leave replacement for the AGM-12 Bullpup.

The original 125-lb (57 kg) high-explosive, shaped-charge warheads have been replaced in later AGM-65s by 300-lb (136 kg) blast-penetration warheads. All versions use the same rocket motor, with maximum launch range depending on target size and seeker performance.

During the Gulf War over 90 per cent of the AGM-65s fired were from A-10As. The Maverick is a very workload-intensive weapon  which pilots of faster aircraft, such as the F-16, found very difficult to employ in combat.

AGM-65A has an electro-optical (television) seeker. After designating the target and ensuring the missile is locked on, the pilot fires the missile and can either select another target.

AGM-65B can locked on a target as an AGM-65A from twice the range.

AGM-65C is not produced.

The USMC became the only user of the AGM-65E semi-active laser (SAL) version. SAL  permits ground troops to designate targets for their close air support.

AGM-65D was the first  infra red version produced, becoming operational during 1986. The advantage of infra red over EO guidance is its ability to used at night and in conditions of  smoke and haze.

For the AGM-65F, the Navy modified the infra red seekers tracking function for anti-ship attacks and incorporated the larger warhead. 

The AGM-65G combines the guidance features of both the D and F with the latter's warhead.