S-200 SA-5 GAMMON Missile

The task of defeating the carriers of cruise missiles, jammers, aircraft of strategic aviation at maximum ranges and heights was solved between 1963 and 1967 with the creation of the S-200 system. Together with the development of many new scientific and technical solutions for the S-200 system, A.A. Raspletin was attached the fundamental importance to the creation of self-homing head for the anti-aircraft guided missile. In the accepted for the armament system S-200 the anti-aircraft guided missile was for the first time equipped with homing equipment.

The S-200 SA-5 GAMMON is a medium to high -altitude surface-to-air missile system. The single-stage missile has four jettisonable, wraparound solid propellant boosters, each of which is is 4.9 m long and 0.48 m in diameter with a single fin spanning 0.35 m from the booster body. The missile is 10.72 m long overall with a wing span of 2.85 m. The main body is 0.85 m in diameter and has a solid fuel dual thrust sustainer rocket motor.

Each missile battalion has one 320 km range P-35M BARLOCK-B E/F-band target search and acquisition radar with an integral D-band IFF system, one 270 km range SQUARE PAIR H-band missile guidance radar, and six trainable semi-fixed single rail launchers.

The missile's minimum range of 60 km is due to the booster burn time and jettison requirements, limiting the system to engagements against relatively large unmaneuverable targets at ranges up to 250 km. Guidance beyond the 60 km booster jettison point is by course correction command signals from the SQUARE PAIR radar with the S-200's own active radar terminal homing seeker head activated near the projected intercept point for final guidance.

The large HE warhead is detonated either by a command signal or the onboard proximity fusing system. When fitted with a nuclear warhead only the command detonation option is used.