S-8KOM UNGUIDED AIRCRAFT ROCKET
NSN: 1315-50-0001549
The S-8KOM unguided aircraft rocket is with a hollow-charge fragmentation warhead and is designed for destruction of ground armoured and unarmoured targets, such as tanks, APCs, missile launchers, radiolocation stations and others, as well as enemy troops.
| CHARACTERISTICS | |
| Caliber, mm | 80 |
| Rocket weight, kg | 11,300 |
| Muzzle velocity, m/s | 55…75 |
| Max. inherent velocity, m/s | 600 |
| Armour penetration, mm | 400 |
| Casualty-producing fragments 3g in size, pcs. | 400 |
| Circular error probable, mils of distance: | |
| – from an aircraft | ≤3 |
| – from a helicopter | ≤8 |
| Safe operational temperature range, °C | -60…60 |
| SYSTEM | |
| B8, B8M, B8M1, B80, B8S7 launcher pods for aircraft, | |
| B8V20A, B8V7 launcher pods for helicopters, and their modifications | |
| PACKING | |
| Dimensions, mm | 1785x315x302 |
| 4 rockets in a case | |
| Gross weight, kg | 68 |