S-8 (rocket)

A S-8 KOM HEAT/FRAG rocket.

The S-8 is a rocket weapon developed by the Soviet Air Force for use by military aircraft. It remains in service with the Russian Air Force and various export customers.

Developed in the 1970s, the S-8 is an 80 mm (3.1 in) rocket used by fighter bombers and helicopters. The system entered service in 1984 and is produced in a variety of subtypes with different warheads, including HEAT anti-armor, high-explosive fragmentation, smoke, and incendiary, as well as the specialized S-8BM runway-destroying munition and the S-8DM fuel-air explosive variants. Each rocket is between 1.5 meters (4 ft 11 in) and 1.7 meters (5 ft 7 in) long and weighs between 11.3 kg (25 lb) and 15.2 kg (33.5 lb), depending on warhead and fuse. Range is 2 to 4 kilometers (1.3 to 2.6 mi).

The S-8 is generally carried in the B series of rocket pods, carrying either seven or 20 rockets.

In 2018, the Russian Aerospace Forces took delivery of several batches of the S-8OFP for trials, successor to the S-8. While both rockets are unguided, the S-8OFP has greater range, a heavier warhead, and a digital fuse.[1]

Rocket specifications

DesignationTypeLength overallLaunch weightWarhead weightRangeNotes
S-8KOHEAT1.57 m11.3 kg3.6 kg
(0.9 kg of explosive)
1.3 to 4 km400 mm versus RHA
S-8KOMHEAT1.57 m11.3 kg3.6 kg
(0.9 kg of explosive)
1.3 to 4 km400 mm versus RHA. Velocity 610 m/s
S-8BPenetrating1.5 m15.2 kg7.41 kg (0.6 kg of explosive)1.2 to 2.2 km800 mm versus reinforced concrete.
S-8BMPenetrating1.54 m15.2 kg7.41 kg (0.6 kg of explosive)1.2 to 2.2 km800 mm versus reinforced concrete. Velocity 450 m/s.
S-8DFAE1.66 m11.6 kg3.8 kg (2.15 kg of explosive)1.3 to 3 km
S-8DMFAE1.7 m11.6 kg3.8 kg (2.15 kg of explosive)1.3 to 3 km5.5–6 kg TNT equivalent. Velocity 590 m/s
S-8DFFAE1.68 m13.4 kg5.5 kg (3.3 kg of explosive)1.3 to 4 km6 kg TNT equivalent. Velocity 500 m/s
S-8 OIlluminating1.63 m12.1 kg4.3 kg4 to 4.5 km2 megacandela flare warhead
S-8 OMIlluminating1.63 m12.1 kg4.3 kg4 to 4.5 km2 megacandela flare warhead burns for 30 seconds. Velocity 545 m/s.
S-8TTandem-HEAT1.7 m13 kg6.6 kg (1.6 kg of explosive)1.3 to 4 kmTandem HEAT 400 mm versus RHA. Velocity 470 m/s
S-8PChaff1.63 m12.3 kg4.5 kg of chaff2 to 3 km
S-8PMChaff1.63 m12.3 kg4.5 kg of chaff2 to 3 km545 m/s velocity.
S-8SFlechette1.612 m13 kg4.3 kg1.2 to 3.5 km2,000 flechettes in 5 bundles
S-8TsMTarget marking1.605 m11.1 kg3.6 kg1.3 to 2 km (heli)
1.3 to 3 km (plane)
target/route marking smoke visible 6 km away

An upgraded version, S-8OFP, has a length of 1.428 m, a weight of less than 17 kg, and a range of 6 km.

See also

References

  1. New Air-ground Rocket For Russian Attack Aircraft. Aviation International News. 10 July 2018.
  • Soviet/Russian Aircraft Weapons Since World War Two, Yefim Gordon, ISBN 1-85780-188-1
  • Mil Mi-24 Hind Attack Helicopter, Yefim Gordon and Dimitri Komissarov, ISBN 1-84037-238-9
  • Jane's Air Launched Weapons Issue 36, Duncan Lennox, ISBN 0-7106-0866-7
  • Warfare.ru S-8 rockets
  • VTTV-99 S-8 rocket specs
  • Army-2018: Zaslon Center presents new 80mm MLRS based on 4x4 UAZ pickup
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