|
SA-2 'Guideline' / S-75 'Dvina' |
|
SA-2 'Guideline' Air Defense Missile |
|
||
Russian Designation: |
S-75 'Dvina' later called 'Volkhov' |
||
Manufacturer: |
KB-1 design bureau |
||
Role: |
Low to High altitude air defense missile |
||
Year Adopted: |
1957 |
||
Weight: |
|
||
Operational Status (1999): |
Russia - Still in use (150 sites) In Service: Afghanistan, Albania, Algeria, Angola, Armenia, Belarus, Bosnia-Herzegovina, Bulgaria, China, Cuba, Czech Republic, Egypt, Ethiopia, Georgia, Hungary, Iran, Iraq, North Korea, Kazakhstan, Kyrgyzstan, Libya, Mozambique, Mongolia, Montenegro, Pakistan, Peru, Poland, Romania, Serbia, Slovakia, Sudan, Syria, Tajikistan, Turkmenistan, Ukraine, Uzbekistan, Vietnam, Yemen |
||
Armament: |
Up to six SA-2 series missiles |
||
Launcher: |
Fixed single rail, trainable |
||
Targeting Radars: |
Fan-Song Series at Battery Level |
Missile Statistics |
|||||||||||
Missile Variants: |
-A, -B, -C, -D, -E, -F |
||||||||||
Length of missile: -A variant -B, -C, -E, -F variants -D variant |
|
||||||||||
Diameter: Booster: Missile: |
|
||||||||||
Launch Weight: -A, -B, -C, -F -D, -E |
|
||||||||||
Propulsion: | Solid fuel booster Storable liquid fuel sustainer rocket motor. |
||||||||||
Guidance: | Proximity or Command Type | ||||||||||
Speed: | Mach 3.5 | ||||||||||
Maximum Range:
-A, -B, -F -C -D, -E |
|
||||||||||
Minimum Range: -A -B -C -D, -E -F |
|
||||||||||
Maximum Altitude:
-A -B -C, -D, -E, -F |
|
||||||||||
Warhead Options:
-A, -B, -C, -E, -F -E -E (optional) |
|
Sources Cited (1) Jane's Land-Based Air Defence 10th ed, edited by Tony Cullen and Christopher F Foss, Jane's Information Group: Surry, United Kingdom, 1997. Print. |