The AS-20 had four steeply swept-back fins, cruciform in cross-section around the midsection of its body. It used a dual-thrustsolid rocket motor, which exhausted through two large nozzles during the boost stage, and a single center line nozzle during the sustain stage. The AS-20 uses a simple MCLOS guidance with the pilot aligning the flares on the missile's rear with the target and controlling the missile in flight after launch with a small joystick sending steering commands to the missile via a radio link. The steering commands steer the missile back to the line-of-sight by thrust vectoring by the movement of one of four metal vanes around the center sustainer nozzle. The missile's internal gyro gives the missile command unit, the correct position of the missile in flight, and to which of the four thrust vanes to actuate at the correct time.