Missile V-75 (SA-2 Guideline)

Description

The V-75 was developed in the Soviet Union during the early 1950s to counter long-range jet bombers. Designed to replace high-altitude anti-aircraft artillery, the system focused on intercepting large, non-maneuvering targets. It entered service in 1957.

The system utilizes a two-stage missile comprising a solid-fuel booster and a storable liquid-fuel upper stage. Guidance is achieved through radio control command signals sent from ground-based computers. The standard warhead is a fragmentation-high explosive type equipped with proximity, contact, and command fusing. The S-75AK variant was developed to carry a nuclear warhead with an estimated yield of 15 kilotons as an alternative to conventional munitions. Ground equipment includes early warning and acquisition radars. Later modifications introduced electronic counter-countermeasure capabilities and passive tracking modes to home in on jamming signals.

The V-75 is widely deployed and has been exported to numerous countries. It remains in service with several operators, including Egypt, North Korea, and Vietnam. The system achieved the first destruction of an aircraft by a surface-to-air missile in 1959 when it struck a Taiwanese RB-57D. It gained further exposure following the 1960 shootdown of a U.S. U-2 reconnaissance aircraft over the Soviet Union and the 1962 destruction of a U-2 during the Cuban Missile Crisis.

During the Vietnam War, the system was used extensively against U.S. aviation, including B-52 bombers. It has seen action in the Six-Day War, the Yom Kippur War, the Iran-Iraq War, and the Gulf War. In the Yemeni Civil War, forces have modified the V-75 for use as a surface-to-surface ballistic missile. China produces domestic versions under the HQ-1 and HQ-2 designations, while Egypt and Iran have produced reverse-engineered or upgraded variants.

Summary

NATO DesignationSA-2 Guideline
CategorySurface-to-Air Missiles
Sub-typeRadar-guided surface-to-air missile
Origin country ๐Ÿ‡จ๐Ÿ‡ณ China ๐Ÿ‡จ๐Ÿ‡ณ Ex-USSR
ManufacturerMKB Fakel
StatusIn service
Year of service1957
Number built4600 units

Technical specifications

WarheadHigh Explosive
Diameter700 mm (27.6 in)
Length10,600 mm (417.3 in)
Flight altitude40,000 m (131,234 ft)
Weight2,300 kg (5,071 lb)
Range 45 km (28 mi)
Max. speed4,100 km/h (Mach 4.1)

Operators

๐Ÿ‡ฆ๐Ÿ‡ซ Afghanistan • ๐Ÿ‡ฆ๐Ÿ‡ด Angola • ๐Ÿ‡ฆ๐Ÿ‡ฑ Albania • ๐Ÿ‡ฆ๐Ÿ‡ฒ Armenia • ๐Ÿ‡ฆ๐Ÿ‡ฟ Azerbaijan • ๐Ÿ‡ง๐Ÿ‡ฌ Bulgaria • ๐Ÿ‡ง๐Ÿ‡ฆ Bosnia and Herzegovina • ๐Ÿ‡ง๐Ÿ‡พ Belarus • ๐Ÿ‡จ๐Ÿ‡ณ China • ๐Ÿ‡จ๐Ÿ‡บ Cuba • ๐Ÿ‡จ๐Ÿ‡ฟ Czech Republic • ๐Ÿ‡ฉ๐Ÿ‡ช Germany • ๐Ÿ‡ช๐Ÿ‡ฌ Egypt • ๐Ÿ‡ช๐Ÿ‡น Ethiopia • ๐Ÿ‡ฌ๐Ÿ‡ช Georgia • ๐Ÿ‡ญ๐Ÿ‡บ Hungary • ๐Ÿ‡ฎ๐Ÿ‡ฉ Indonesia • ๐Ÿ‡ฎ๐Ÿ‡ณ India • ๐Ÿ‡ฎ๐Ÿ‡ท Iran • ๐Ÿ‡ฎ๐Ÿ‡ถ Iraq • ๐Ÿ‡ฐ๐Ÿ‡ฟ Kazakhstan • ๐Ÿ‡ฐ๐Ÿ‡ฌ Kyrgyzstan • ๐Ÿ‡ฑ๐Ÿ‡พ Libya • ๐Ÿ‡ฒ๐Ÿ‡ฒ Myanmar • ๐Ÿ‡ฒ๐Ÿ‡ณ Mongolia • ๐Ÿ‡ฒ๐Ÿ‡ฟ Mozambique • ๐Ÿ‡ต๐Ÿ‡ฐ Pakistan • ๐Ÿ‡ต๐Ÿ‡ฑ Poland • ๐Ÿ‡ฐ๐Ÿ‡ต North Korea • ๐Ÿ‡ท๐Ÿ‡ด Romania • ๐Ÿ‡ท๐Ÿ‡บ Russia • ๐Ÿ‡ธ๐Ÿ‡ฉ Sudan • ๐Ÿ‡ธ๐Ÿ‡ด Somalia • ๐Ÿ‡ธ๐Ÿ‡ฐ Slovakia • ๐Ÿ‡ธ๐Ÿ‡พ Syria • ๐Ÿ‡น๐Ÿ‡ฏ Tajikistan • ๐Ÿ‡บ๐Ÿ‡ฆ Ukraine • ๐Ÿ‡บ๐Ÿ‡ฟ Uzbekistan • ๐Ÿ‡ป๐Ÿ‡ณ Vietnam • ๐Ÿ‡พ๐Ÿ‡ช Yemen • ๐Ÿ‡ณ๐Ÿ‡ฑ Ex-Yugoslavia
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