Malo o municiji.
APFSDS-TArmour-piercing fin-stabilized discarding sabot tracer or APFSDS-T rounds. Typically used against other modern tanks.
3VBM3/3BM9/10Entered service in 1962. The projectile is Maraging steel.
Country of origin: Soviet Union
Projectile dimension: 410 mm 10: 1 L/d
Projectile weight (including sabot): 5.67 kg
Projectile weight: 3.6 kg
Muzzle velocity: 1800 m/s
Muzzle energy: 5.8 MJ
Penetration: 245 mm at 0° at 2000 m, 80 mm at 60° at 2000 m, (energy at 2000 m is 4.2 MJ)
3VBM6/3BM12/13Entered service (estimated) in 1968. Essentially the same as the 3BM9 projectile with a tungsten carbide plug.
Country of origin: Soviet Union
Projectile dimension: 410 mm 10: 1 L/d
Projectile weight (including sabot): 5.67 kg
Projectile weight: 3.6 kg
Muzzle velocity: 1800 m/s
Muzzle energy: 5.8 MJ
Penetration: 280 mm at 0° at 2000 m, 110 mm at 60° at 2000 m, (energy at 2000 m is 4.2 MJ)
3VBM7/3BM15/16 Entered service (estimated 1972). A slightly longer 3BM12 projectile.
Country of origin: Soviet Union
Projectile dimension: 435 mm 12: 1 L/d
Projectile weight (including sabot): 5.9 kg
Projectile weight: 3.9 kg including 2.9 kg and 0.27 kg tungsten carbide plug
Muzzle velocity: 1780 m/s
Muzzle energy: 6.2 MJ
Certified Penetration: 310 mm at 0° at 2000 m, 120 mm at 60° at 2000 m,
Interestingly, the 'predicted penetration' is 150mm at 60° at 2000 m,
3VBM8/3BM17/18Entered service (estimated 1972). An export version of the 3BM-15 without the tungsten carbide plug. Hence, it is an all-steel penetrator with inferior performance.
Country of origin: Soviet Union
Projectile dimension: 450 mm 12: 1 L/d
Projectile weight (including sabot): 5.9 kg
Projectile weight: 3.9 kg
Muzzle velocity: 1760 m/s
Muzzle energy: 6.2 MJ
Certified Penetration: 290 mm at 0° at 2000 m, 110 mm at 60° at 2000 m,
3VBM9/3BM22/23Entered service 1976. Tungsten carbide penetrator core sheathed in steel.
Country of origin: Soviet Union
Projectile dimension: 400 mm 11: 1 L/d
Projectile weight (including sabot): 6.55 kg
Projectile weight: 4.485 kg
Muzzle velocity: 1760 m/s
Muzzle energy: 7.0 MJ
Penetration: 380 mm at 0° at 2000 m, 170 mm at 60° at 2000 m,
3VBM10/3BM29/30Entered service 1982. Depleted Uranium-nickel-iron alloy sheathed in steel.
Country of origin: Soviet Union
Projectile dimension: 450 mm 12: 1 L/d - including 250 mm core.
Projectile weight (including sabot): 6.55 kg
Projectile weight: 4.85 kg
Muzzle velocity: 1700 m/s
Muzzle energy: 7.0 MJ
Penetration: 430 mm at 0° at 2000 m, 210 mm at 60° at 2000 m,
3VBM11/3BM26/27Entered service 1983. Tungsten-nickel-iron alloy core sheathed in steel.
Country of origin: Soviet Union
Projectile dimension: 395 mm 11: 1 L/d
Projectile weight (including sabot): 7.05 kg
Projectile weight: 4.8 kg
Muzzle velocity: 1720 m/s
Muzzle energy: 7.5 MJ
Penetration: 410 mm at 0° at 2000 m, 200 mm at 60° at 2000 m,
3VBM13/3BM32/33Entered service in 1985. The projectile is a depleted uranium-nickel-zinc alloy, sheathed in steel.
Country of origin: Soviet Union
Projectile dimension: 380 mm 13: 1 L/d
Projectile weight (including sabot): 7.05 kg
Projectile weight: 4.85 kg
Muzzle velocity: 1700 m/s
Muzzle energy: 7.0 MJ
Penetration 500 mm at 0° at 2000 m, 250 mm at 60° at 2000 m,
3VBM17/3BM42 (3BM44) Entered service in 1986. The projectile is a tungsten alloy core sheathed in steel.
Country of origin: Soviet Union
Projectile dimension: 452 mm 15: 1 L/d
Round weight: 20.4 kg
Projectile weight: 4.85 kg [3]
Projectile weight (including sabot): 7.05 kg
Muzzle velocity: 1700 m/s
Muzzle energy: 7.0 MJ
Penetration: 450 mm at 0° at 2000 m, 220 mm at 60° at 2000 m.
3VBM19/3BM42M (3BM44M "Lekalo")Entered service in 1994 Utilising an improved penetrator and a new Sabot. Reported to be tungsten alloy.
Country of origin: Russia
Projectile dimension: 570 mm 22: 1 L/d
Round weight: ?
Projectile weight (including sabot): 6.95 kg
Muzzle velocity: 1750 m/s
Muzzle energy: 7.4 MJ (estimated - assuming 4.85 kg projectile)
Penetration: 650 mm at 0° at 2000 m
3VBM??/3BM46 (3BM48 "Svinets")Entered service in 1991 Utilising a new Sabot. Reported to be Uranium alloy.
Country of origin: Russia
Projectile dimension: 546 mm : 22? L/d
Round weight: 4.85 kg
Projectile weight (including sabot): ?.?? kg
Muzzle velocity: 1700 m/s
Muzzle energy: ?.? MJ
Penetration: 650 mm at 0° at 2000 m, 300 mm at 60° at 2000 m
3VBM??/3BM46 (3BM48 "Свинец-2")Entered service : Unknown. Utilising a new Sabot. Reported to be tungsten alloy.
Country of origin: Russia
Projectile dimension: ? mm
Round weight: Unknown
Projectile weight (including sabot): ?.?? kg
Muzzle velocity: 1700? m/s
Muzzle energy: ?.? MJ
Penetration: 750?? mm at 0° at 2000?? m
HEAT-FSHigh-explosive anti-tank fin stabilised or HEAT-FS rounds. Typically used against lighter or older tanks and Armoured personnel carriers.
3VBK7/3BK12Entered service 1962.
Country of origin: Soviet Union
Projectile dimension: 680 mm
Projectile weight: 19 kg
Max dispersion: 0.21 mil (0.21 mrad)
Muzzle velocity: 905 m/s
Charge: shaped charge, Steel liner, A-IX-1 (RDX phlegmatized with 5% wax), I-238 detonator
Penetration: 420 mm RHA at 0 degrees.
3BK12MEntered service 1968. Uses improved 3V-15 detonator.
Country of origin: Soviet Union
3VBK10/3BK14Entered service 1968.
Country of origin: Soviet Union
Projectile dimension: 680 mm
Projectile weight: 19 kg
Max dispersion: 0.21 mil (0.21 mrad)
Muzzle velocity: 905 m/s
Charge: shaped charge, Steel liner, phlegmatized 75% HMX, 25% TNT; 3V-15 detonator
Charge weight: 1.62 kg
Penetration: 450 mm RHA at 0 degrees.
3BK14MImproved version, replacing steel liner with a copper liner.
3VBK16/3BK18Entered service estimated 1975.
Country of origin: Soviet Union
Round weight: 29.0 kg
Projectile dimension: 680 mm
Projectile weight: 19 kg
Max dispersion: 0.21 mil (0.21 mrad)
Muzzle velocity: 905 m/s
Charge: shaped charge, copper liner, phlegmatized 75% HMX, 25% TNT; 3V-15 detonator
Penetration: 500 mm RHA at 0 degrees.
3BK18MImproved warhead. Entered service estimated 1978. Introduces wave shaping booster.
Country of origin: Soviet Union
Projectile weight: 19.02 kg
Muzzle velocity: 905 m/s
Penetration: 550 mm RHA at 0 degrees
3VBK17/3BK21Entered service estimated 1980. Enhancements to improve reliability of the copper jet formation.
Country of origin: Soviet Union
Projectile dimension: 680 mm
Projectile weight: 19 kg
Max dispersion: 0.21 mil (0.21 mrad)
Muzzle velocity: 905 m/s
Charge: shaped charge, copper liner, phlegmatized 75% HMX, 25% TNT; 3V-15 detonator
Penetration: 550 mm RHA at 0 degrees.
3BK21BEntered service estimated 1982. Depleted uranium Liner to enhance penetration of advanced composite armours like Chobham.
Country of origin: Soviet Union
Projectile dimension: 680 mm
Projectile weight: 19 kg
Muzzle velocity: 905 m/s
Penetration: 750 mm RHA at 0 degrees.
3VBK21/3BK25Entered service estimated 1985.
Country of origin: Soviet Union
Muzzle velocity: 905 m/s
3VBK25/3BK29Entered service estimated 1988.
Country of origin: Soviet Union
Round weight: 28.4 kg
Projectile dimension: 680 mm
Projectile weight: 18.4 kg
Muzzle velocity: 915 m/s
Penetration: 350mm to 400mm RHA at 60 degree tandem charge
3VBK27?/3BK29MFirst seen publicly in 1998. Reportedly a triple charge warhead.
Country of origin: Russia
Projectile weight: 18.4 kg
Charge weight: 1.62 kg
Muzzle velocity: 915 m/s
Penetration: Estimated at 800 mm triple charge HEAT.
HE-FRAG-FSHigh Explosive Fragmentation Fin Stabilised. General purpose rounds, for use against infantry, bunkers and light vehicles and other 'soft' targets.
3VOF22/3OF19 Entered service in 1962. Uses the 3V-21 detonator (mass = 0.431 kg, reliability = 0.98). The 90% lethal zone for infantry is reported to be 40 m wide and 20 m deep.[3]
Country of origin: Soviet Union
Round weight: 33.0 kg
Projectile weight: 23.0 kg
Muzzle velocity: 850 m/s
Max dispersion: 0.23 mil (0.23 mrad)
Charge weight: 3.148 kg
Charge: TNT
3VOF36/3OF26 Entered service in 1970. Uses the 3V-21 detonator (mass = 0.431 kg, reliability = 0.98). The projectile creates between 600 and 2,000 fragments.
Country of origin: Soviet Union
Round weight: 33.0 kg
Projectile weight: 23.0 kg
Muzzle velocity: 850 m/s
Max dispersion: 0.23 mil (0.23 mrad)
Charge weight: 3.148 kg
Charge: A-IX-2 (73% RDX, 23% aluminium powder, phlegmatized with 4% wax) 3.4 kg
ATGW/ATGM9M112 Kobra The 9K112 Kobra (NATO reporting name is AT-8 Songster) is also fired from the 125 mm main guns of the T-64 and T-80 series of tanks.[6]
Country of origin: Soviet Union
Projectile weight: 23.2 kg
Warhead weight: 4.5 kg
Guidance system: Radio-command guided
Range: 100 – 4000 metres
Penetration: Estimated at 600 millimetres (24 in) tandem charge HEAT.
9M119 RefleksThe 9M119 Svir and 9M119M Refleks (NATO reporting name: AT-11 Sniper) anti-tank guided missile has semi-automatic laser beam-riding guidance and a tandem hollow-charge HEAT warhead. It has an effective range of 75 m to 5000 m, and takes 17.6 seconds to reach maximum range. Refleks can penetrate about 900 millimetres (35 in) of steel armour and can also engage low-flying air targets such as helicopters.[6]
Country of origin: Soviet Union
Projectile weight: 16.5 kg
Warhead weight: 4.5 kg
Guidance system: Laser-beam riding
Range: 75 – 5000 metres
Penetration: Estimated at 900 millimetres (35 in) tandem charge HEAT.
https://en.wikipedia.org/wiki/125_mm_smoothbore_ammunition