BM-25 (multiple rocket launcher)

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BM-25
TypeMultiple rocket launcher
Place of originUSSR
Service history
Used byUSSR
South Yemen
Production history
DesignerNII-88
Designed1953
Produced1957-1960
Specifications
Mass18,145 kg (40,003 lb)
Length9.8 m (32 ft 2 in)
Width2.7 m (8 ft 10 in)
Height3.5 m (11 ft 6 in)
Crew8-12
ShellLength: 5.8 m (19 ft 0 in)
Weight: 455 kg (1,003 lb)
Caliber250 mm (9.8 in)
Barrels6
Elevation0° - 55°
Traverse
Effective firing range30 km (19 mi)
Maximum firing range55 km (34 mi)
EngineYaMZ-206B 6-cylinder
205 HP diesel
SuspensionKrAZ-214 6x6 truck chassis
Operational
range
530 km (330 mi)
Maximum speed 55 km/h (34 mph)

The BM-25 Korshun (Kite) as its Russian (GRAU designation 2K5) name was a multiple rocket launcher designed in the Soviet Union. It was capable of launching 3R7 250 mm rockets from six launch tubes. The support vehicle is a YAZ-214.

Development

The system was developed in scientific research institute NII-88 in 1953. Its rockets were propelled by a mix of kerosene and nitric acid. It has a range of 55km but was inaccurate.

Use

Due to severe inaccuracy of the rocket, only a small quantity had been produced in USSR from 1957 to 1960. It was exported to South Yemen, which used them against North Yemen.

See also

Wikimedia Commons has media related to BM-25.

Notes

  1. ^ a b c Foss, Christopher (1977). Jane's pocket book of towed artillery. New York: Collier. p. 27. ISBN 0020806000. OCLC 911907988.
  2. ^ a b Prenatt & Hook 2016, p. 27.
  3. ^ Prenatt & Hook 2016, p. 28.
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