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S-125 Neva/Pechora

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Introductions:

The S-125 Neva/Pechora is a Soviet surface-to-air missile system that was designed by Aleksei Isaev to complement the S-25 and S-75. It has a shorter effective range and lower engagement altitude than either of its predecessors and also flies slower, but due to its two-stage design it is more effective against more maneuverable targets. It is also able to engage lower flying targets than the previous systems, and being more modern it is much more resistant to ECM than the S-75. The 5V24 (V-600) missiles reach around Mach 3 to 3.5 in flight, both stages powered by solid fuel rocket motors. The S-125, like the S-75, uses radio command guidance. The naval version of this system has the NATO reporting name SA-N-1 Goa and original designation M-1 Volna

The S-125 was first deployed between 1961 and 1964 around Moscow, augmenting the S-25 and S-75 sites already ringing the city, as well as in other parts of the USSR. In 1964, an upgraded version of the system, the S-125M "Neva-M" and later S-125M1 "Neva-M1" was developed. The original version was designated SA-3A by the US DoD and the new Neva-M named SA-3B and (naval) SA-N-1B. The Neva-M introduced a redesigned booster and an improved guidance system. The S-125 was not used against U.S. forces in Vietnam, because the Soviets feared that China (after the souring of Sino-Soviet relations in 1960), through which most, if not all of the equipment meant for North Vietnam had to travel, would try to copy the missile.

(About the one that shot down the F-117:)

A Yugoslav Army 250th Air Defense Missile Brigade 3rd battery equipped with S-125 system shot down a F-117 Nighthawk stealth attack aircraft on March 27, 1999 during the Kosovo War (the only recorded downing of a stealth aircraft) near village Budjanovci, about 45 km from Belgrade. The pilot LT.COL. Darrell Patrick Zelko ejected and was later found by US search and rescue forces. An S-125 also shot down a NATO F-16 fighter on May 2 (its pilot; Lt. Col David L. Goldfein, the commander of 555th Fighter Squadron, managed to eject and was later rescued by a combat search-and-rescue (CSAR) mission).

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General Characteristics

  • Created On iOS
  • Wingspan 37.2ft (11.3m)
  • Length 75.5ft (23.0m)
  • Height 29.2ft (8.9m)
  • Empty Weight 62,113lbs (28,174kg)
  • Loaded Weight 62,113lbs (28,174kg)

Performance

  • Wing Loading N/A
  • Wing Area 0.0ft2 (0.0m2)
  • Drag Points 26959

Parts

  • Number of Parts 200
  • Control Surfaces 0
  • Performance Cost 530