Company Products

Rocket design Unguided aviation rocket S-8КОМ-ВЕ consists of a warhead with a mounted piezo-electrical fuse system and a rocket motor. The rocket motor is composed of solid ballistic fuel and in the temperature range from 213 К to 333 К has the following characteristics: sum impulse of the thrust - from 5394 N.s to 5984 N.s; working time - from 0,45 s to 1,3 s. A modern method for manufacturing from pre-shaped aluminum pipes is being used for the construction of the housing. Intended use Unguided aviation rocket S-8КОМ-ВЕ is from the class "air to surface" and it is intended for destruction of: armored ground targets (tanks, self-propelled artillery, armored vehicles and armored personnel carriers); unarmored ground targets (specialized machines, radar stations, airplanes and helicopters on the ground etc.); enemy troops; Main data Caliber, mm 80 Length, mm 1542 max Weight, kg:    - of the rocket 11,3    - of the warhead 3,6    - of the explosive 1,0 Explosive brand GEKFOL-5 Designation of the solid rocket propellant brand BINOM or BNK-R Maximal velocity, m/s 600 Armour penetration capability, mm not less than 400 Quantity of programmed fragments 3 g in weight not less than 400 Firing distance, m 1300 - 4000 Temperature range of combat usage, К (°С) from 213 to 333 (-60 to 60) Probable deviation of the technical dispersion of the rockets in the picture plane upon firing    - From an airplane at speed of 600 to 1200 km/h, mrad not more than 3    - From a helicopter at speed of 200 to 300 km/h, mrad not more than 8 Warhead - KO With cumulative and fragmentation action Fuse system -V-5KP1 Piezoelectric, with contact action List of aviation carriers Unguided aviation rocket S-8КОМ-ВЕ is used as ammunition for Russian-made airplanes and helicopters. The S-8KOM-BE Unguided aviation rocket is intended for launching from the following launcher pods: B-8 rocket pod with 20 tubes and its modifications B-8-0, B-8M, and B-8M1; B-8V20-A rocket pod with 20 tubes; B-8V7 and B-8S7 rocket pod with 7 tubes. Storage and transportation The unguided aviation rockets are stored in wooden packing in closed warehouses. In field conditions they are stored under sheds or tarpaulins that prevent direct moisture or sunlight. The unguided aviation rockets S-8KOM-BE are transported in their packaging during all kinds of transport. Packaging Unguided aviation rocket S-8КОМ-ВЕ 4 rockets in a wooden box Size of the packaging, mm 1770х300х275 Volume, m3 0,146 Gross weight, кg 68 Safety class 1.1F UN 0180

Rocket design Unguided aviation rocket S-8КОМ-BE PRACTICAL consists of a warhead and a rocket motor. The rocket motor is composed of solid ballistic fuel and in the temperature range from 213 К to 333 К has the following characteristics: sum impulse of the thrust - from 5394 N.s to 5984 N.s; working time - from 0,45 to 1,3s A modern method for manufacturing from pre-shaped aluminum pipes is being used for the construction of the housing. Intended use Unguided aviation rocket S-8КОМ-ВЕ PRACTICAL is from the class "air to surface" and is used for training the personnel of different Air Forse units to use S-8KOM, S-8KOM-BE and S-8KOM-MBE by firing at firing range targets by airplanes and helicopters. The S-8KOM-BE PRACTICAL rocket marks the hit by flash and smoke. Main data Caliber, mm 80 Rocket length, mm 1522 max Rocket weight, kg 11,3 Weight of the warhead, kg 3,6 Weight of the smoke and flash generating module, kg 0,240 Smoke and flash visibility range when the rocket meets the target and actuation of the front part (at meteorological visibility of 1 km), km not less than 4,5 Maximal velocity, m/s 600 Firing distance, m 1300 - 4000 Temperature range of combat usage, К (°С) from 213 to 333 (-60 to 60) Probable deviation of the technical dispersion of the rockets in the picture plane upon firing:    - From an airplane at speed of 600 to 1200 km/h, mrad not more than 3    - From a helicopter at speed of 200 to 300 km/h, mrad not more than 8 Fuse system – FPZ-17 Piezoelectric, duplicated by inertial action. Protective type, with distant arming secured by clockworks, not influenced by climate conditions. With electronic protection against non-standard circumstances during flight time. List of aviation carriers Unguided aviation rocket S-8КОМ-ВЕ PRACTICAL is used as ammunition for Russian-made airplanes and helicopters. The S-8KOM-BE PRACTICAL Unguided aviation rocket is intended for launching from the following launcher pods: B-8 rocket pod with 20 tubes and its modifications B-8-0, B-8M, and B-8M1; B-8V20-A rocket pod with 20 tubes; B-8V7 and B-8S7 rocket pod with 7 tubes. Storage and transportation The unguided aviation rockets are stored in wooden packing in closed warehouses. In field conditions they are stored under sheds or tarpaulins that prevent direct moisture or sunlight. The unguided aviation rockets S-8KOM-BE PRACTICAL are transported in their packaging during all kinds of transport. Packaging Unguided aviation rocket S-8КОМ-ВЕ PRACTICAL 4 rockets in a wooden box Size of the packaging, mm 1770х300х275 Volume, m3 0,146 Gross weight, кg 68 Safety class 1,1F UN 0180

Rocket design Unguided aviation rocket S-8КОМ-ВЕ INERT consists of a inert warhead and a rocket motor. The rocket motor is composed of solid ballistic fuel and in the temperature range from 213 К to 333 К has the following characteristics: sum impulse of the thrust - from 5394 N.s to 5984 N.s; working time - from 0,45 s to 1,3 s. A modern method for manufacturing from pre-shaped aluminum pipes is being used for the construction of the housing. Intended use Unguided aviation rocket S-8КОМ-ВЕ INERT is from the class "air to surface" and is used for training the personnel of different Air Forse units to use S-8KOM, S-8KOM-BE and S-8KOM-MBE by firing at firing range targets by airplanes and helicopters. Main data Caliber, mm 80 Rocket length, mm 1542 max Rocket weight, kg 11,3 Weight of the warhead, kg 3,6 Maximal velocity, m/s 600 Firing distance, m 1300 - 4000 Temperature range of combat usage, К (°С) from 213 to 333 (-60 to 60) Probable deviation of the technical dispersion of the rockets in the picture plane upon firing:    - From an airplane at speed of 600 to 1200 km/h, mrad not more than 3    - From a helicopter at speed of 200 to 300 km/h, mrad not more than 8 Warhead - KO  INERT is a mass-size inert evaluation model of a warhead КО. List of aviation carriers Unguided aviation rocket S-8КОМ-ВЕ INERT is used as ammunition for Russian-made airplanes and helicopters. The S-8KOM-BE INERT Unguided aviation rocket is intended for launching from the following launcher pods: B-8 rocket pod with 20 tubes and its modifications B-8-0, B-8M, and B-8M1; B-8V20-A rocket pod with 20 tubes; B-8V7 and B-8S7 rocket pod with 7 tubes. Storage and transportation The unguided aviation rockets are stored in wooden packing in closed warehouses. In field conditions they are stored under sheds or tarpaulins that prevent direct moisture or sunlight. The unguided aviation rockets S-8KOM-BE INERT are transported in their packaging during all kinds of transport. Packaging Unguided aviation rocket S-8КОМ-ВЕ INERT 4 rockets in a wooden box Size of the packaging, mm 1770х300х275 Volume, m3 0,146 Gross weight, кg 68 Safety class 1,2C UN 0502

Rocket design Unguided aviation rocket S-8КОМ-MВЕ consists of a warhead with a mounted piezo-electrical fuse system and a rocket motor. The rocket motor is composed of solid ballistic fuel and in the temperature range from 213 К to 333 К has the following characteristics: sum impulse of the thrust - from 5394 N.s to 5984 N.s; working time - from 0,45 s to 1,3s. A modern method for manufacturing from pre-shaped aluminum pipes is being used for the construction of the housing. Intended use Unguided aviation rocket S-8КОМ-MВЕ is from the class "air to surface" and it is intended for destruction of: armored ground targets (tanks, self-propelled artillery, armored vehicles and armored personnel carriers); unarmored ground targets (specialized machines, radar stations, airplanes and helicopters on the ground etc.); enemy troops; Main data Caliber, mm 80 Length, mm 1522 max Weight, kg:    - of the rocket 11,3    - of the warhead 3,6    - of the explosive 1,0 Explosive brand PBXN-6 or GEKFOL-5 Designation of the solid rocket propellant brand BINOM or BNK-R Maximal velocity, m/s 600 Armor penetration capability, mm not less than 400 Quantity of programmed fragments 3 g in weight not less than 400 Firing distance, m 1300 - 4000 Temperature range of combat usage, К (°С) from 213 to 333 (-60 to 60) Probable deviation of the technical dispersion of the rockets in the picture plane upon firing:    - From an airplane at speed of 600 to 1200 km/h, mrad not more than 3    - From a helicopter at speed of 200 to 300 km/h, mrad not more than 8 Warhead - WH-80HCF With cumulative and fragmentation action. Fuse system – FPZ-17 Piezoelectric, duplicated by inertial action. Protective type, with distant arming secured by clockworks, not influenced by climate conditions. With electronic protection against non-standard circumstances during flight time. List of aviation carriers Unguided aviation rocket S-8КОМ-MВЕ is used as ammunition for Russian-made airplanes and helicopters. The S-8KOM-MBE Unguided aviation rocket is intended for launching from the following launcher pods: B-8 rocket pod with 20 tubes and its modifications B-8-0, B-8M, and B-8M1; B-8V20-A rocket pod with 20 tubes; B-8V7 and B-8S7 rocket pod with 7 tubes. Storage and transportation The unguided aviation rockets are stored in wooden packing in closed warehouses. In field conditions they are stored under sheds or tarpaulins that prevent direct moisture or sunlight. The unguided aviation rockets S-8KOM-MBE are transported in their packaging during all kinds of transport. Packaging Unguided aviation rocket S-8КОМ-MВЕ 4 rockets in a wooden box Size of the packaging, mm 1770х300х275 Volume, m3 0,146 Gross weight, кg 68 Safety class 1,1F UN 0180

Rocket design Unguided aviation rocket S-8DМ-ВЕ consists of a warhead with solid volume-detonating mixture, a mounted piezo-electrical fuse system and a rocket motor. The rocket motor is composed of solid ballistic fuel and in the temperature range from 213 К to 333 К has the following characteristics: sum impulse of the thrust - from 5394 N.s to 5984 N.s; working time - from 0,45s to 1,3s. The warhead has a thermobaric action and at detonation a high-energy cloud is formed from the components of the volume-detonating mixture. The fuse system ensures safe operation during handling of the rocket and reliability when firing at all kinds of surfaces, even in case of a ricochet angle upon meeting the target. Intended use Unguided aviation rocket S-8DМ-ВЕ is from the class "air to surface" and it is intended for destruction of: Unarmoured ground targets (specialized machines, radar stations, aircraft and helicopters on the ground, warehouses for fuel handling materials etc.); The enemy manpower located in trenches, ditches, pits, caves and other similar shelters. Main data Caliber, mm 80 Length, mm 1615 max Weight, kg:    - of the rocket 11,6    - of the warhead 3,8    - of the explosive 2,15 Explosive brand ETB-10 Designation of the solid rocket propellant brand BINOM or BNK-R Maximal velocity, m/s 590 TNT equivalent, kg TNT 5,0 - 5,5 Firing distance, m 1300 - 4000 Temperature range of combat usage, К (°С) from 213 to 333 (-60 to 60) Probable deviation of the technical dispersion of the rockets in the picture plane upon firing:    - From an airplane at speed of 600 to 1200 km/h, mrad not more than 3    - From a helicopter at speed of 200 to 300 km/h, mrad not more than 8 Warhead – WH-80TB With thermobaric action. In the center of the explosion excess pressure is created and temperature above 2200°C Fuse system – FPZ-17 Piezoelectric, duplicated by inertial action. Protective type, with distant arming secured by clockworks, not influenced by climate conditions. With electronic protection against non-standard circumstances during flight time. List of aviation carriers Unguided aviation rocket S-8DМ-ВЕ is used as ammunition for Russian-made airplanes and helicopters. The S-8DM-BE Unguided aviation rocket is intended for launching from the following launcher pods: B-8 rocket pod with 20 tubes and its modifications B-8-0, B-8M, and B-8M1; B-8V20-A rocket pod with 20 tubes; B-8V7 and B-8S7 rocket pod with 7 tubes. Storage and transportation The unguided aviation rockets are stored in wooden packing in closed warehouses. In field conditions they are stored under sheds or tarpaulins that prevent direct moisture or sunlight. The unguided aviation rockets S-8DM-BE are transported in their packaging during all kinds of transport. Packaging Unguided aviation rocket S-8DМ-ВЕ 4 rockets in a wooden box Size of the packaging, mm 1770х300х275 Volume, m3 0,146 Gross weight, кg 68 Safety class 1,1F UN 0180

Rocket design Unguided aviation rocket S-8HEF-BE consists of a warhead with a mounted piezo-electrical fuse system and a rocket motor. The rocket motor is composed of solid ballistic fuel and in the temperature range from 213 К to 333 К has the following characteristics: sum impulse of the thrust - from 5394 N.s to 5984 N.s; working time - from 0,45 s to 1,3 s. A modern method for manufacturing from pre-shaped aluminum pipes is being used for the construction of the housing. Intended use Unguided aviation rocket S-8HEF-BE is from the class "air to surface" and it is designed for destruction of unarmored targets and manpower - via hollow high explosive and fragmentation action. Main data Caliber, mm 80 Length, mm 1522 max Weight, kg:    - of the rocket 11,3    - of the warhead 3,6    - of the explosive 1,0 Explosive brand A-IX-20 Designation of the solid rocket propellant brand BINOM or BNK-R Maximal velocity, m/s 600 Quantity of programmed fragments 2 g in weight not less than 700 Firing distance, m 1300 - 4000 Temperature range of combat usage, К (°С) from 213 to 333 (-60 to 60) Probable deviation of the technical dispersion of the rockets in the picture plane upon firing:    - From an airplane at speed of 600 to 1200 km/h, mrad not more than 3    - From a helicopter at speed of 200 to 300 km/h, mrad not more than 8 Warhead – WH-80HEF With high explosive and fragmentation action Fuse system – FPZ-17 Piezoelectric, duplicated by inertial action. Protective type, with distant arming secured by clockworks, not influenced by climate conditions. With electronic protection against non-standard circumstances during flight time. List of aviation carriers Unguided aviation rocket S-8HEF-BE is used as ammunition for Russian-made airplanes and helicopters. The S-8HEF-BE Unguided aviation rocket is intended for launching from the following launcher pods: B-8 rocket pod with 20 tubes and its modifications B-8-0, B-8M, and B-8M1; B-8V20-A rocket pod with 20 tubes; B-8V7 and B-8S7 rocket pod with 7 tubes. Storage and transportation The unguided aviation rockets are stored in wooden packing in closed warehouses. In field conditions they are stored under sheds or tarpaulins that prevent direct moisture or sunlight. The unguided aviation rockets S-8HEF-BE are transported in their packaging during all kinds of transport. Packaging Unguided aviation rocket S-8HEF-BE 4 rockets in a wooden box Size of the packaging, mm 1770х300х275 Volume, m3 0,146 Gross weight, кg 68 Safety class 1,1F UN 0180

The aerial target simulator IVC-2MD is a training combat rocket and it is designed to simulate modem, small size, high speed means of air attack in the radiolocation and optical bands of wavelength and to emit active jamming in the frequency range of 7,5 GHz to 15 GHz. It is used for training of combat units equipped with air defense means operating at medium and short distances, as well as in development and testing of new anti-aircraft missile systems. It is shot from a launcher BM-21 of Multiple rocket system 9K51 "Grad" or a launcher PU-2MD and it has the same ballistic characteristics as the regular rocket 9M22U (M210F). Structure: The aerial target simulator IVC-2MD consists of: front part - ensuring the implementation of all simulating functions of the device; fuse - providing the input parameters of the ballistic flight path and ensuring the reliable actuation of the device mounted in the front part; source of infrared radiation - 4 tracers ind.9X44; source of electricity The installation of the sources of infrared radiation and the source of electricity in the front part, as well as the joining of the front part and the fuse, is carried out directly on the firing position. Main features Caliber, mm 122 Weight, kg not more than 66,7 Flight distance, km not less than 15 Flight altitude range, km 2 - 5 Speed of flight in the area of use, m/s not more than 320 Maximum duration of flight, s 60 Temperature range, oK 213 - 323 Weight of the front part, kg 18,5 Visibility distance for simulation of aerial target in the optic range of the wavelength (in meteorological visibility at least 1 km away), km not less than 5 Duration of visibility in the optic range, s not less than 35 Effective Reflective Surface (at frequency of 15 GHz radar) at imitating aerial target in the radiolocation range, sq.m 0,5 - 1,5 Range of jamming emission, GHz 7,5 - 15 Duration of jamming emission (5 s after the start), s not less than 45 Packaging The front part is packed in a wooden case - 1 piece Overall dimensions of the case, mm 910x290x290 The fuse is packed in a wooden case - 1 piece Overall dimensions of the case, mm 2810x280x252