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S-25 Rocket

SKU: MD-P00750·Defense & Defense Systems·受注生産

S-25 Rocket
S-25 Rocket

概要

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

技術仕様

Specifications. 主な仕様: 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。

技術仕様 — 1 groups
主な仕様: 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。

技術仕様

Specifications

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

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