
With the the wide PCB traces from the 1950’s.
The missile was constructed in two separate portions for the nose and tail. The nose contained the guidance receivers which translated instructions into commands for the electro-pnuematic actuators for the four small delta wing control fins arranged around the nose. The tail section held the two tracking flares and larger wings to maintain flight and help prevent the airframe from rolling in flight. The main roll prevention was provided by a gyroscope controlling the front control fins.
The Bullpup used a Manual Command Line Of Sight guidance system with roll-stabilization. In flight, the pilot or weapons operator tracked the Bullpup by watching two flares on the boat-tail and used a control joystick to steer it toward the target using radio signals. The goal was to direct the missile so that it remained on the line between the pilot and the target.
After launching the Bullpup, best accuracy was maintained by continuing to fly the same track, so that the pilot could sight down the smoke trail and steer the missile from directly behind as much as possible. Unfortunately, one problem quickly discovered by pilots in Vietnam was that gunners on the ground could simply fire at the smoke trail of the missile’s flare and have a fairly good chance of hitting the aircraft that had launched—and was still guiding—the missile. Thus, to try to protect their own aircraft, the pilot would “jig” slightly off of the missile’s path and hopefully avoid the anti-aircraft fire.
Development of the AGM-12 Bullpup began in the early 1950s, after the Korean War sparked a demand for more precise, guided, weapon systems that could hit targets which were usually more difficult to hit with conventional ordnance.

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