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After trials of the S-25 Berkut in 1955, the Soviet Union started development of the RS-25 Dal long-range missile system with the V-400/5V11 missile. It was initially assigned the "SA-5" designation in the West [4] and codenamed "Griffon", but the project was abandoned in 1964. [5] The SA-5 designation was then assigned to the S-200.
U.S. DoD designations for SA-N series naval surface-to-air missiles, with Soviet designations. Note that these are not standard NATO names, NATO uses the regular SA series for naval SAMS also, however the US DoD refers to them by these names: SA-N-1 Goa (4К90 Volna) [SA-3] SA-N-2 Guideline (М-2 Volkhov-M) [SA-2] SA-N-3 Goblet (4K60/4K65 ...
A pair of S-300 missiles being launched. A surface-to-air missile (SAM), also known as a ground-to-air missile (GTAM) or surface-to-air guided weapon (SAGW), is a missile designed to be launched from the ground or the sea to destroy aircraft or other missiles.
This Wikipedia page lists various surface-to-air missiles.
The 2K11 Krug (Russian: 2К11 Круг; English: 'circle') is a Soviet and now Russian medium-range, medium-to-high altitude surface-to-air missile (SAM) system. The system was designed by NPO Novator and produced by Kalinin Machine Building Plant.
The 9K32 Strela-2 (Russian: Cтрела, lit. 'Arrow'; NATO reporting name SA-7 Grail) is a light-weight, shoulder-fired, surface-to-air missile or MANPADS system. It is designed to target aircraft at low altitudes with passive infrared-homing guidance and destroy them with a high-explosive warhead.
The 9K38 Igla (Russian: Игла́, "needle", NATO reporting name SA-18 Grouse) is a Soviet/Russian man-portable infrared homing surface-to-air missile (SAM) system. A simplified, earlier version is known as the 9K310 Igla-1 (NATO: SA-16 Gimlet), and the latest variant is the 9K338 Igla-S (SA-24 Grinch).
The Vertical Launch – Short Range Surface to Air Missile, or VL-SRSAM is a quick reaction surface-to-air missile developed by the Indian Defence Research and Development Organisation (DRDO). [ 5 ] During mid-course flight, the missile uses fibre-optic gyroscope based inertial guidance mechanism while in terminal phase uses active radar homing .