S-25 Rocket

Обзор

The S-25 rocket (Russian: C-25) is a series of aerial rocket systems developed by the Soviet Air Force and used by military aircraft against semi-hard and hard ground targets. It still serves in the Russian Air Force and various export customers. Date of development: Mid-1960s - 1975 Manufacturer: KB Tochmash Date of production :1975 - present S-25 rocket Basic Specifications Weight :480 kg (1,058.22 lb) Length:3,310-3,800 mm (130.31-149.61 in) Warhead: 300-420 mm (11.81-16.54 in) Effective range: 3,000-11,000 m (3,280.84-12,029.75 yd, 9,842.52-36,089.24 ft, 1.86-6.84 mi) Warhead: 150-190 kg (330.69-418.88 lb) explosive yield Detonation mechanism: trigger fuse or proximity fuse Wingspan :600 mm (23.62 in) Speed: 511-700 m/s, about 1.5-2.06 Mach Guidance system: unguided/laser guidance system S-25F: Models equipped with high explosive warheads, range 2,000-3,000 m. S-25O: Model equipped with fragmentation warhead and radio proximity fuze. S-25O-PU: Model equipped with a cone charge warhead. S-25OF: Model with high blaster warheads. (Russian: Осколочно-фугасный снаряд). S-25OFM: Model for enhanced targets. S-25M: A modernized version of the S-25OF. S-25MD: Modernized version with extended range of 4,000-5,000 m. S-25L: laser-guided version, Bunker buster, ground-penetrating warhead version with a range of 7,000 m. S-25LD: laser-guided and extended range version with a range of 11,000 m. S-25TV: Model with Television guidance head, mainly for export. S-25IRS: Model with infrared guidance head. S-25A: The model of active radar guidance head with Ku-band (18-40 GHZ) active radar guidance. S-25SE: Equipped with the Glonass system

Технические характеристики

Основные характеристики: Date of development Mid-1960s - 1975, Date of production 1975 - present, Weight 480 kg (1,058.22 lb), Length 3,310-3,800 mm (130.31-149.61 in), Body 250 mm (9.84 in), Warhead 300-420 mm (11.81-16.54 in), Effective range 3,000-11,000 m (3,280.84-12,029.75 yd, 9,842.52-36,089.24 ft, 1.86-6.84 mi), Detonation mechanism trigger fuse or proximity fuse, Engine Rocket engine, Wingspan 600 mm (23.62 in), Speed 511-700 m/s, about 1.5-2.06 Mach, Guidance system unguided/laser guidance system, S-25F Models equipped with high explosive warheads, range 2,000-3,000 m., S-25O Model equipped with fragmentation warhead and radio proximity fuze., S-25O-PU Model equipped with a cone charge warhead., S-25OF Model with high blaster warheads. (Russian: Осколочно-фугасный снаряд)., S-25OFM Model for enhanced targets., S-25M A modernized version of the S-25OF., S-25MD Modernized version with extended range of 4,000-5,000 m., S-25L laser-guided version, Bunker buster, ground-penetrating warhead version with a range of 7,000 m., S-25LD laser-guided and extended range version with a range of 11,000 m., S-25TV Model with Television guidance head, mainly for export., S-25IRS Model with infrared guidance head., S-25A The model of active radar guidance head with Ku-band (18-40 GHZ) active radar guidance., S-25SE Equipped with the Glonass system.

Технические характеристики

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