The basic Kh-59 model is released from the carrier plane, after which the first stage fires, a solid fuel accelerator in the tail. Now the stabilizers located in the front of the missile unfold, with wings and rudder in the rear. Driven by the second stage cruise rocket engine, the Kh-59 cruises at an altitude of about 7 metres above water or above ground with the help of a
radar altimeter. It can be launched at speeds of at altitudes of and has a
CEP of . The
36MT turbofan engine developed for the Kh-59M class of missiles is manufactured by
NPO Saturn of Russia. Target coordinates are fed into the missile before launch, and the initial flight phase is conducted under inertial guidance. At a distance of from the target the television guidance system is activated. An operator aboard the aircraft visually identifies the target and locks the missile onto it. ==Operational history==