The original SA-2 Guideline design was engineered to track down and destroy the less-maneuverable high-altitude American bombers, more precisely - the Air Force's stalwart, the B-52 Stratofortress. The capabilities of the Guideline system were highly valued, so much so that all other primary air defense systems (with the exception of those marking Moscow), were replaced by the newer SA-2's. By 1965, no fewer than 1,000 SA-2 Guideline launch sites had been established throughout the Soviet Empire and its satellite locations with a large contingent residing in the Soviet-controlled East Germany.
The first confirmed downing of an aircraft by the SA-2 system was of a Taiwanese reconnaissance aircraft of the RB-57 type, destroyed in 1959 over China. Successes continued to follow the system including the notable downing of Gary Power's U-2 Spy plane that reached the global headlines (more than one missile was actually launched and the aircraft was hit several times before going down). This single act resulted in a re-thinking of military and reconnaissance planning when dealing with high-altitude Soviet air defense systems.
During the Vietnam conflict with America, Soviet-supplied SA-2's to the North Vietnamese were responsible for aggressively targeting and destroying US Navy, Air Force and Marine aircraft. As a direct response, the United States was forced to develop counter-weapons systems to help combat the very serious SA-2 threat.
Despite advancements in Electronic CounterMeasure (ECM) systems and tactics, the SA-2 system still enjoyed relative success throughout the conflict and afterwards (some running through modernization programs to help extend the service life of the system). Never the less, the SA-2 Guideline would eventually begin giving way to the more advanced SA-10 series of surface-to-air missile systems.
The base system combines fragmentation warhead with proximity, contact and command fusing capability mounted to a two-stage solid rocket fuel booster system. The warhead weighs in at roughly 434 pounds and can be fitted with an alternative nuclear-capable warhead if need be. Range is reported to be up to 30 miles and the missile system can reach upwards of 60,000 feet.
NOTE: Specifications shown above are for the SA-2A Guideline model of the SA-2 Guideline series of air defense missiles.
(Showcased structural values pertain to the SA-2 (Guideline) / S-75 Dvina production model)
1 x two-stage solid-fuel booster with upper-stage liquid fuel.
(Showcased powerplant information pertains to the SA-2 (Guideline) / S-75 Dvina production model)
1,864 mph (3,000 kph)
19 miles (30 km)
(Showcased performance values pertain to the SA-2 (Guideline) / S-75 Dvina production model; Compare this entry against any other in our database)
1 x 35ft, 5,041lb surface-to-air missile (various available warheads). Targeting by radar system.
Ammunition: 1 x 35ft, 5,041lb surface-to-air missile (various available warheads).
(Showcased armament details pertain to the SA-2 (Guideline) / S-75 Dvina production model)
SA-2 - NATO Reporting Designation
SA-2A - Featured with Fan Song-A radar system and utilizes either V-750 or V-750V missiles.
S-75 Dvina - Russian designation of the SA-2A model.
SA-N-2A - Naval Version
S-75M-2 Volkhov-M - Russian designation of the SA-N-2A model.
SA-2B - Features Fan Song-B radar system and utilizes V-750VK or V-750VN missiles.
S-75 Desna - Russian designation of the SA-2B model.
SA-2C - Features Fan Song-C radar system and utilizes V-750m missiles.
S-75M Volkhov - Russian designation of the SA-2C model.
SA-2D - Featured with Fan Song-E radar system and utilizes V-750SM missiles.
SA-2E - Featured with Fan Song-E radar system and utilizes V-750AK missiles.
SA-2F - Featured with Fan-Song-F radar system and utilizes V-750SM missiles.
C-75 - Russian Reporting Designation
HQ-1 - Chinese-produced Variant
HQ-2 - Chinese-produced Variant
HY-2 - Chinese-produced Variant of upgraded SA-2 base model.
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